Tag Archives: Atlas

Canelo APOLOGIZES TO CALEB PLANT admits he just learned what mother f’er means & ROASTS Teddy Atlas! – Fight Hub TV

  1. Canelo APOLOGIZES TO CALEB PLANT admits he just learned what mother f’er means & ROASTS Teddy Atlas! Fight Hub TV
  2. Moving on up: Is history on Jermell Charlo’s side when he faces Canelo Alvarez at super middleweight? – ESPN ESPN
  3. Teddy Atlas Makes Bold Canelo-Charlo Prediction: “He’ll Win By Split Decision” Boxing Social
  4. Saul ‘Canelo’ Alvarez, Jermell Charlo arrive at MGM Grand for fight on Saturday KTNV 13 Action News Las Vegas
  5. Jermell Charlo RIPS Canelo’s demeanor! I’M NOT HERE TO KISS YOUR A**, I’M HERE TO FIGHT! Fight Hub TV
  6. View Full Coverage on Google News

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Boston Dynamics’ Atlas robot grows a set of hands, attempts construction work

Boston Dynamics’ Atlas—the world’s most advanced humanoid robot—is learning some new tricks. The company has finally given Atlas some proper hands, and in Boston Dynamics’ latest YouTube video, Atlas is attempting to do some actual work. It also released another behind-the-scenes video showing some of the work that goes into Atlas. And when things don’t go right, we see some spectacular slams the robot takes in its efforts to advance humanoid robotics.

As a humanoid robot, Atlas has mostly been focused on locomotion, starting with walking in a lab, then walking on every kind of unstable terrain imaginable, then doing some sick parkour tricks. Locomotion is all about the legs, though, and the upper half seemed mostly like an afterthought, with the arms only used to swing around for balance. Atlas previously didn’t even have hands—the last time we saw it, there were only two incomplete-looking ball grippers at the end of its arms.

This newest iteration of the robot has actual grippers. They’re simple clamp-style hands with a wrist and a single moving finger, but that’s good enough for picking things up. The goal of this video is moving “inertially significant” objects—not just picking up light boxes, but objects that are so heavy they can throw Atlas off-balance. This includes things like a big plank, a bag full of tools, and a barbell with two 10-pound weights. Atlas is learning all about those “equal and opposite forces” in the world.

Like everything in robotics, picking up and carrying an object is more complicated than it seems. Atlas has to figure out where it is in the world in relation to the object it’s picking up, come up with a grasping plan for the hands, and lift and manipulate the object, all while calculating how this extra bit of mass will affect its balance. As Boston Dynamics software engineer Robin Deits explains in the video, “When we’re trying to manipulate something like a plank, we have to just make pretty educated guesses about where is the plank, how fast is it moving, how do we need to move the arms to cause the plank to spin 180 degrees very quickly, and if we get those estimates wrong we end up doing silly things and falling over.”

Atlas isn’t just clumsily picking things up and carrying them, though. It’s running, jumping, and spinning while carrying heavy objects. At one point it jumps and throws the heavy toolbox up to its construction partner, all without losing balance. It’s doing all this on rickety scaffolding and improvised plank walkways, too, so the ground is constantly moving under Atlas’ feet with every step. Picking up stuff is the start of teaching the robot to do actual work, and it looks right at home on a rough-and-tumble construction site. The simple claw grippers mean Atlas crushes everything it picks up, though, with objects like the plank showing visible damage where the hands dug into it. Maybe the next set of experiments will teach Atlas to be less of a hulking gorilla.

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Watch a Boston Dynamics Atlas Robot Grab and Throw, Just Like People Can

Boston Dynamics’ Atlas machines are aiming to be the humans of the robot world when it comes to physical abilities. They can already do parkour and gymnastics, but recent upgrades have added new skills that make the bots even more like people than before.

When we saw Atlas slaying a parkour course in 2021, it had stubby appendages for hands. Today’s Atlas, star of a Boston Dynamics video released Wednesday, has grippers and a sense of show-robot-ship. 

The video plays out as a work site vignette with a human who’s forgotten his tools while up on a high platform. The worker calls for Atlas to fetch his tool bag. The robot gamely builds a bridge, grabs the bag, hops to a higher spot and slings the bag up to its boss. It then performs a gymnastics-style dismount. 

The video is a demonstration of the pincher-style hand grippers and the robot’s ability to alter its environment and accurately toss a heavy object to complete a task. A behind-the-scenes video goes into detail on how the robot is perceiving and manipulating items.

Atlas has come a long way. It was less than a decade ago that a CNET writer commented on an early version of the robot being “terrible at karate.” Boston Dynamics uses Atlas as a test bed to try out technologies and new robotic capabilities.

Another much-discussed humanoid robot is the AI-focused Tesla Optimus robot, which is a very different animal (excuse me — robot) from Atlas. It’s also in an earlier stage of development, so don’t expect any Atlas-Optimus face-offs in the near future. Both machines show how humanity is working toward the reality of the sci-fi dream of robots made in our own image.

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Senescence atlas reveals an aged-like inflamed niche that blunts muscle regeneration

Animal models

C57Bl/6 (WT), p16-3MR (donated by J. Campisi)18, dystrophic mdx (DBA/2-background) and mdx/p16-3MR (dystrophic mdx mice crossed with p16-3MR mice) were bred and aged at the animal facility of the Barcelona Biomedical Research Park (PRBB), housed in standard cages under 12 h–12 h light–dark cycles and fed ad libitum with a standard chow diet. All of the experiments followed the principle of the ‘three Rs’—replacement, reduction and refinement according to Directive 63/2010 and its implementation in the Member States. All of the procedures had authorization from the PRBB Animal Research Ethics Committee (PRBB-CEEA) and the local government (Generalitat de Catalunya) and were conducted according to the European Directive 2010/63/EU and Spanish regulations RD 53/2013. Both male and female mice were used in each experiment unless stated otherwise. Live colonies were maintained and genotyped according to the Jackson Laboratories’ guidelines and protocols. The mice were housed together, their health was monitored daily for sickness symptoms (not age-related weight loss and so on) and they were euthanized immediately at the clinical end point when recommended by veterinary and biological service staff members. Mice were randomly allocated to experimental or treatment groups. No blinding was used. No statistical methods were used to predetermine the sample size. For PCR genotyping, the following primers were used: p16-3MR-1, 5′-AACGCAAACGCATGATCACTG-3′; and p16-3MR-2, 5′-TCAGGGATGATGCATCTAGC-3′. Positive mice show a band at 202 bp.

Human biopsies

Human muscle biopsy samples from the vastus lateralis muscle of patients undergoing surgery were obtained from the biobank of the EU/FP7 Myoage Consortium, as previously reported5,6. Ethical approval was received from the local ethics committees at each of the five research centres of the Consortium. All of the participants provided written informed consent and were medically screened before participation. The biobanked muscle tissue had been directly frozen in melting isopentane and stored at −80 °C until analysed. Damaged areas were identified by morphological criteria on the basis of the presence of infiltrating mononuclear cells. Data are from female patients aged 69, 82, 80, 89 or 85 years old; the average age was 81 ± 7.5 years.

In vivo treatments

Quercetin (USP, 1592409; 50 mg kg1) and dasatinib (LC Laboratories, D-3307; 5 mg kg1) were administered orally (by gavage). Control mice were administered with an equal volume of vehicle (10% ethanol, 30% polyethilenglicol and 60% phosal). GCV (Sigma-Aldrich, G2536-100MG; 25 mg kg1) was injected intraperitoneally (i.p.). Anti-CD36 antibodies (Cayman Chemical, 10009893; 10 µg or 20 µg in young mice and 20 µg in old mice) diluted in PBS was administered via i.p., and control mice received an equal dose of IgA control antibodies (Southern Biotech/Bionova, 0106-14). Treatments with GCV, senolytics and CD36 were administered daily for 4–7 consecutive days as indicated in the figure legends. NAC (Sigma-Aldrich, A9165; 0.01 g ml−1) was added into drinking water (exchanged every 3 days) 1 week before muscle injury and was prolonged until euthanasia. SIS3 (Sigma-Aldrich, S0447-5MG; 10 mg kg1) in PBS and bortezomib (Teva, TH000345/LF2.3; 0.5 mg kg1) in 10% DMSO diluted in PBS were administered i.p. (from 1 to 5 d.p.i.). For long-term treatments, 3-month-old mdx and mdx/p16-3MR mice were administered with D+Q or GCV, respectively, twice a week for 2 months.

Muscle regeneration

Mice were anaesthetized with ketamine–xylazine (80 and 10 mg kg1 respectively; i.p.) or isoflurane. Regeneration of skeletal muscle was induced by intramuscular injection of CTX (Latoxan, L8102; 10 µM) as described previously51. At the indicated times after injury, the mice were euthanized and the muscles were dissected, frozen in liquid-nitrogen-cooled isopentane, and stored at −80 °C until analysis.

Heterografting

Heterografting experiments were performed according to the protocol described previously52. In brief, the EDL muscle was removed from the anatomical bed of either p16-3MR or WT mice and was transplanted onto the surface of the TA muscle of the p16-3MR or WT recipient mouse or vice versa. Muscle grafts were collected on day 7 after transplantation.

Muscle force measurement

Ex vivo force measurements of EDL muscles were assessed as previously described53 using and 300B apparatus (Aurora Scientific). Force was normalized per muscle area, determined by dividing the muscle mass by the product of length and muscle density of (1.06 mg mm−3), to calculate the specific force (mN mm−2).

p16-3MR Renilla luciferase reporter assay

In vivo, Renilla luciferase activity was measured in the TA, quadriceps and gastrocnemius muscles of p16-3MR mice. Anaesthetized mice were injected intramuscularly with coelenterazine H (PerkinElmer, 760506) and luciferase activity was immediately measured using the IVIS Lumina III (PerkinElmer) system. In vitro, Renilla luciferase activity was measured from the cryopreserved diaphragm and TA muscles using the Dual-Luciferase Reporter Assay Kit (Promega, E1910). The signal was measured using the luminometer Centro LB 960 (Berthold Technologies) and values were normalized to the total protein extracted measured using Bradford method (Protein Assay, Bio-Rad, 500–0006), and the damaged area was measured after haematoxylin and eosin (H&E) staining.

Cell isolation by flow cytometry

Muscles were mechanically disaggregated and incubated in Dulbecco’s modified Eagle’s medium (DMEM) containing liberase (Roche, 177246) and dispase (Gibco, 17105-041) at 37 °C with agitation for 1–2 h. When required, SPiDER-β-gal reagent (Dojindo, SG02; 1 µM) was added during the second hour. The supernatant was then filtered and cells were incubated in lysis buffer (BD Pharm Lyse, 555899) for 10 min on ice, resuspended in PBS with 2.5% fetal bovine serum (FBS) and counted. BV711-conjugated anti-CD45 (BD, 563709; 1:200), APC-Cy7-conjugated anti-F4/80 (BioLegend, 123118; 1:200), PE-conjugated anti-α7-integrin (Ablab, AB10STMW215; 1:200), APC-conjugated anti-CD31 (eBioscience, 17-0311-82; 1:200) and PE-Cy7-conjugated anti-SCA1 (BioLegend, 108114; 1:200) antibodies were used to isolate MCs (CD45+F4/80+), SCs (α7-integrin+CD45F4/80CD31) and FAPs (SCA1+CD45F4/80α7-integrinCD31). PE-Cy7-conjugated anti-CD45 antibodies (BioLegend, 103114) were used to isolate CD45-positive and CD45-negative populations (Extended Data Fig. 1h). SPiDER-β-gal (SPiDER) was used to isolate senescent cells (SPiDER+) from non-senescent cells (SPiDER) of each cell type (Extended Data Figs. 1h and 4a) (Supplementary Table 1). Cells were sorted using the FACS Aria II (BD) system. Cell lineage was confirmed by specific-cell marker expression (Extended Data Fig. 4b–d). Isolated cells were used either for RNA extraction, cell cultures, engraftments, proliferation assays or plated onto glass slides (Thermo Fisher Scientific, 177402) for immunostaining and SA-β-gal analysis.

To isolate ROShigh and ROSlow populations, the digested muscle was stained with CellRox Green reagent (Invitrogen, C10444; 5 µM) according to the manufacturer’s protocol and PE-Cy7-conjugated anti-CD45 (BioLegend, 103114; 1:200), PE-Cy7-conjugated anti-CD31 (BioLegend, 102418; 1:200), PE-conjugated anti-α7-integrin (Ablab, AB10STMW215; 1:200) and APC-conjugated anti-SCA1 (BioLegend, 108111; 1:200) antibodies to separate SCs (α7-integrin+CD45CD31) and FAPs (SCA1+CD45α7-integrinCD31) (Supplementary Table 1). CellRoxhigh and CellRoxlow cells were sorted using the FACS Aria II (BD) system. Isolated cells were used for cell cultures and proliferation assays. The acquisition was performed using the BD FACS Diva software.

Senescent cell transplantation

Cells transplants were performed as described previously5, following an adapted protocol54. FACS-isolated SPiDER+ and SPiDER cells were collected, resuspended in 20% FBS DMEM medium, labelled with Vybrant Dil Cell Labelling solution (Invitrogen, V22889) according to manufacturer instructions and injected into the TA muscles of recipient mice that were either uninjured or previously injured using the freeze crush method 2 days before55. The cell-type proportions of MCs, SCs and FAPs were controlled in the transplanted SPiDER+ and SPiDER populations. Each TA muscle was engrafted with 10,000 cells, except when each senescent cell type was transplanted separately (Fig. 5k), where 5,000 cells were engrafted. Engrafted muscles were collected and processed for muscle histology 4 days after cell transplantation.

RNA interference

Freshly sorted cells or C2C12 cells (ATCC, CRL-1772) were transfected with siRNA targeting Cd36 (On-Target plus SmartPool, Dharmacon, L-062017-00-0005; 5 nM) or unrelated sequence as control (On-Target plus non-targeting siRNA Pool, Dharmacon, D-001810-10-05; 5 nM) using the DharmaFect protocol (Dharmacon, T-2003-02). Target sequences for Cd36 siRNA were as follows: 5′-CCACAUAUCUACCAAAAUU-3′, 5′-GAAAGGAUAACAUAAGCAA-3′, 5’-AUACAGAGUUCGUUAUCUA-3’, 5’-GGAUUGGAGUGGUGAUGUU-3’. Freshly sorted cells after incubation with siRNAs for 3 hours were washed and engrafted.

Cytokine array

Cytokine antibody arrays (R&D Systems, ARY028; Abcam, ab193659) were used according to the manufacturer’s protocol. For cells, freshly sorted cells were cultured for 24 h in serum-free DMEM. Cell culture supernatants were collected, centrifuged and incubated with the membranes precoated with captured antibodies. For tissue interstitial fluid, skeletal muscles of mice were dissected and slowly injected with a PBS solution with a Complete Mini EDTA-free protease inhibitor cocktail (Roche, 11836170001). The PBS exudate was then recovered centrifuged and incubated with the membranes precoated with captured antibodies. The membranes were then incubated with detection antibodies, streptavidin–HRP and Chemi Reagent Mix. The immunoblot images were captured and visualized using the ChemiDoc MP Imaging System (Bio-Rad) and the intensity of each spot in the captured images was analysed using the publicly available ImageJ software.

Proliferation assays

To assess proliferation in vivo, muscles were injured by local CTX injection, and the mice were administered with ethynyl-labelled deoxyuridine (EdU, Invitrogen, A10044; 25.5 mg kg1; i.p.) 2 h before euthanasia at 4 d.p.i. The muscles were collected and processed for immunofluorescence staining in tissue slides or cell isolation by FACS. EdU-labelled cells were detected using the Click-iT EdU Imaging Kit (Invitrogen, C10086). EdU-positive cells were quantified as the percentage of the total number of cells analysed. In vitro proliferation was quantified on freshly sorted SCs, seeded in 20% FBS Ham’s F10 medium supplemented with b-FGF (Peprotech, 100-18B-250UG; 2.5 ng ml1) in collagen-coated plates. After 3 days of culture, SCs were pulse-labelled with bromodeoxyuridine (BrdU, Sigma-Aldrich, B9285-1G; 1.5 μg ml1) for 1 h. BrdU-labelled cells were detected by immunostaining using rat anti-BrdU antibodies (Abcam, AB6326, 1:500) and a specific secondary biotinylated donkey anti-rat antibody (Jackson Immunoresearch, 712-066-150, 1:250). Antibody binding was visualized using Vectastain Elite ABC reagent (Vector Laboratories, PK-6100) and 3,3′-diaminobenzidine. BrdU-positive cells were quantified as the percentage of the total number of cells analysed.

Transwell assay

SCs were freshly isolated from regenerating muscle tissue at 3 d.p.i. and plated onto 24-well plates (Falcon, 353047) in 20% FBS DMEM supplemented with b-FGF. Subsequently, medium or freshly sorted SPiDER+ and SPiDER cell populations (Fig. 5i) or etoposide-induced senescent C2C12 cells (Fig. 6i) were seeded on a 0.4-µm-pore-size cell culture insert (Falcon, 353495) using the same medium. After 3 days of culture, a proliferation assay was performed on SCs with BrdU labelling as described above.

In vitro treatments

ROShigh and ROSlow SCs and FAPs were freshly isolated from regenerating muscle at 24 h after injury, seeded and cultured in the presence of NAC (10 mM) or vehicle for 3 days. After the treatment, cells were fixed and further processed for staining. C2C12 cells maintained in 10% FBS DMEM were treated with etoposide (Sigma-Aldrich, E1383, 1 µM) for 5 days to induce senescence and were collected for RNA extraction and RT–qPCR. Cells were stained with a β-galactosidase staining kit (as described below) to confirm their senescent state.

Cell staining

SA-β-galactosidase (SA-β-gal) activity was detected in freshly sorted cells and cell cultures using the senescence β-galactosidase staining kit (Cell signalling, 9860) according to the manufacturer’s instructions. Lipid droplets were stained with Oil Red O (Sigma-Aldrich, O0625) according to manufacturer instructions. ROS levels were measured by immunofluorescence using CellRox Green reagent (Invitrogen, C10444; 5 µM) according to the instructions. TUNEL assays were performed using the In Situ Cell Death Detection Kit, Fluorescein (Roche, 11684795910), cells treated with DNase were used as a positive control of the staining according to the manufacturer’s description.

Muscle histology, immunofluorescence and immuno-FISH

Muscles were embedded in OCT solution (TissueTek, 4583), frozen in isopentane cooled with liquid nitrogen and stored at −80 °C until analysis. Muscle cryosections (thickness, 10 μm) were collected and stained for SA-β-gal (AppliChem, A1007,0001), H&E (Sigma-Aldrich, HHS80 and 45235), MYH3 (DSHB, F1.652), Sirius Red (Sigma-Aldrich, 365548) or used for immunofluorescence (Supplementary Table 1). The CSA of H&E- and MYH3-antibody-stained sections, the percentage of muscle area positive for Sirius Red staining and the number of SA-β-gal+ cells were quantified using Image J. Double immunofluorescence was performed by the sequential addition of each primary and secondary antibody using positive and negative controls. The sections were air-dried, fixed, washed on PBS and incubated with primary antibodies according to the standard protocol after blocking with a high-protein-containing solution in PBS for 1 h at room temperature. Subsequently, the slides were washed with PBS and incubated with the appropriate secondary antibodies and labelling dyes. Telomere immuno-FISH was performed after γH2AX immunofluorescence staining with telomeric PNA probe (Panagene, F1002-5) as described previously56.

Digital image acquisition

Digital images were acquired using an upright DMR6000B microscope (Leica) with a DFC550 camera for immunohistochemical colour pictures; a Thunder imager 3D live-cell microscope (Leica Microsystems) with hardware autofocus control and a Leica DFC9000 GTC sCMOS camera, using HC PL FLUOTAR ×10/0.32 PH1 ∞/0.17/ON257C and HC PL FLUOTAR ×20/0.4 CORR PH1 ∞/0-2/ON25/C objectives; a Zeiss Cell Observer HS with a ×20 and x40 air objective and a Zeiss AxioCam MrX camera; and a Leica SP5 confocal laser-scanning microscope with HCX PL Fluotar ×40/0.75 and ×63/0.75 objectives. The different fluorophores (three or four) were excited using the 405, 488, 568 and 633 nm excitation lines. The acquisition was performed using the Leica Application (v.3.0) or LAS X (v.1.0) software (Leica) or Zeiss LSM software Zen 2 Blue.

RNA isolation and RT–qPCR

Total RNA was isolated from snap-frozen muscles using the miRNAeasy Mini Kit (Qiagen, 1038703). PicoPure (Thermo Fisher Scientific, KIT0204) was used for RNA isolation from sorted cells. For RT–qPCR experiments, DNase digestion of 10 mg of RNA was performed using 2 U DNase (Qiagen, 1010395). cDNA was synthesized from total RNA using SuperScript III Reverse Transcriptase (Invitrogen, 18080-044). For gene expression analysis in freshly sorted SCs, FAPs and MCs, cDNA was pre-amplified using the SsoAdvanced PreAmp Supermix (Bio-Rad, 172-5160) according to the manufacturer’s instructions. qPCR reactions were performed as described previously57. Reactions were run in triplicate, and automatically detected threshold cycle values were compared between samples. Transcripts of the Rpl7 housekeeping gene were used as the endogenous control, with each unknown sample normalized to Rpl7 content (a list of the primers used in this study is provided in Supplementary Table 2).

RNA-seq sample and library preparation

Sequencing libraries were prepared directly from the lysed cells, without a previous RNA-extraction step. RNA reverse transcription and cDNA amplification were performed using the SMART-Seq v4 Ultra Low Input RNA Kit for Sequencing from Clontech Takara. The Illumina Nextera XT kit was used for preparing the libraries from the amplified cDNA. Libraries were sequenced using the Illumina HiSeq 2500 sequencer (51 bp read length, single-end, around 20 million reads).

Bulk RNA-seq data preprocessing

Sequencing reads were preprocessed using the nf-core/rnaseq (v.1.2) pipeline58. Read quality was assessed using FastQC (v.0.11.8)59. Trim Galore (v.0.5.0)60 was used to trim sequencing reads, eliminating the remains of Illumina adaptors and discarding reads that were shorter than 20 bp. The resulting reads were mapped onto the mouse genome (GRCm38, Ensembl61 release 81) using HiSAT2 (v.2.1.0)62 and quantified using featureCounts (v.1.6.2)63. Reads per kilobase per million mapped reads (RPKM) and transcripts per million (TPM) gene expression values were calculated from the trimmed mean of M-values (TMM)-normalized counts per million (CPM) values using the Bioconductor package edgeR (v.3.30.0)64 and R (v.4.0.0)65. Differential gene expression analysis and PCA were performed using the Bioconductor package DESeq2 (v.1.28.1)66. Variance-stabilizing transformation of count data was applied to visualize the sample-to-sample distances in PCA. Genes were considered to be differentially expressed if showed an adjusted P < 0.05.

Functional profiling of cell subpopulations

Functional enrichment analysis of the subsets of differentially expressed genes was performed using g:Profiler web server67 with the g:SCS significance threshold, ‘Only annotated’ statistical domain scope, and canonical pathway KEGG68, Reactome69 and Wiki Pathways70 sets. For each gene subset, the top five significant gene sets were selected for representation.

GSEA

The RPKM matrix after the removal of low-count genes (edgeR (v.3.30.0)64) was used as an input for the GSEA (v.4.0.3) software71. We used the signal-to-noise metric to rank the genes, 1,000 permutations with the gene set permutation type and weighted enrichment statistics. Gene set sizes were chosen as 15–500 for MSigDB 7.0 GO:BP and 10–1,000 for MSigDB 7.0 canonical pathways (BioCarta, KEGG, PID, Reactome and WikiPathways)72. Gene sets passing the FDR < 0.25 threshold were processed for further analysis. Network representation and clustering of GSEA results were performed using EnrichmentMap (v.3.2.1)73 and AutoAnnotate (v.1.3.2)74 for Cytoscape (v.3.7.2)75 with the Jaccard coefficient set to 0.25.

Functional profiling of SASP

We checked whether upregulated genes (DESeq2 adjusted P < 0.05 and log2[fold change] > 0) from each Sen versus NSen comparison can be expressed in a form of secreted proteins by combining the evidence from multiple data sources: GO76 cellular component (GO:CC), Uniprot77, VerSeDa78, Human Protein Atlas79 and experimental data reporting SASP10,80. The genes encoding extracellular (GO:CC) and/or secreted (other sources) products, with evidence from at least one source, were included in the final list of SASP genes (1,912 in total). Functional enrichment analysis was performed using the g:Profiler web server67 with the g:SCS significance threshold, ‘Only annotated’ statistical domain scope, and canonical pathway sets from KEGG, Reactome and Wiki Pathways. Gene sets passing the FDR < 0.05 threshold were processed for further analysis. Network representation and clustering of the g:Profiler results were performed using EnrichmentMap (v.3.2.1) and AutoAnnotate (v.1.3.2) for Cytoscape (v.3.7.2) with the Jaccard coefficient set to 0.25.

Comparative enrichment analysis of senescent cells and previously published ageing datasets

We used the minimum hypergeometric test implemented in the R package mHG (v.1.1)81 for the comparative enrichment analysis of senescent cells and previously published ageing datasets: mouse36, rat (Gene Expression Omnibus (GEO): GSE53960), African turquoise killifish (GEO: GSE69122), and human (GTEx82 v6p). Data processing and analysis were performed as described previously36.

scRNA-seq and analysis

scRNA-seq was performed using the Chromium Single Cell 3′ GEM, Library & Gel Bead Kit v3, 16 rxns (10x Genomics, PN-1000075) according to the manufacturer’s instructions and targeting a recovery of 5,000 cells per dataset. Each dataset was obtained with a sample size of two mouse biological replicates. The libraries were constructed as instructed in the manufacturer’s protocol and sequenced using the MGI DNBSEQ-T7 sequencer platform. The average read depth across the samples was 15,551 per cell. Sequencing reads were processed with STARsolo (v.2.7.3a)83 using the mouse reference genome mm10 (GENCODE vM23 (ref. 84)).

From the filtered barcode and count matricesm, downstream analysis was performed using R (v.4.0.3). Quality control, filtering, data clustering, visualization and differential expression analysis were performed using the Seurat (v.4.0.3) and DoubletFinder (v.2.0) R packages85,86. Datasets were processed following Seurat standard integration protocol according to the tutorial instructions. Genes expressed in less than 3 cells and cells with fewer than 500 features, less than 2,000 transcripts and more than 20% reads mapping to mitochondrial genes as well as cells identified as doublets by DoubletFinder were removed. PCA was performed for dimensionality reduction and the first 30 components were used for UMAP embedding and clustering.

ATAC-seq sample and library preparation

Omni-ATAC-seq was performed in freshly sorted cells as described previously87,88. After the transposition reaction and purification, the transposed fragments were amplified using 50 μl of PCR mix (20 µl of DNA, 2.5 µl of custom Nextera PCR primers 1 and 2, and 25 µl of KAPA HiFi HS Ready Mix for a total of 15 cycles). The PCR amplification conditions were as follows: 72 °C for 5 min; 95 °C for 30 s; 15 cycles of 95 °C for 10 s, 63 °C for 30 s and 72 °C for 60 s; and a final extension at 72 °C for 5 min. After PCR amplification, the libraries were purified, and the size was selected from 150 to 800 bp using AMPure XP beads. Paired-end sequencing was performed with 50 cycles on the Illumina NovaSeq 6000 platform.

Bulk ATAC-seq data preprocessing

Read quality was assessed using FastQC (v.0.11.8). All adaptors were removed using Fastp (v.0.21.0)89. The clean reads were then aligned to mm10 mouse genome assembly using Bowtie2 (v.2.2.5)90 with the settings ‘–very sensitive’. Low-mapping-quality reads were removed using samtools (v.1.3.1)91 with the settings ‘-q 30’. BigWig files were generated using deeptools (v.3.3.1)92 with the settings ‘-normalizeUsing CPM’. Peaks were called using Macs2 (v.2.1.0)93 with the options ‘–nomodel –keep-dup -q 0.01’. For differential accessibility analysis, union peak sets were created using Bedtools (v.2.29.2)94, reads corresponding to each region were assigned by FeatureCounts. Differentially accessible peaks were identified using DESeq2 (v.1.24.0) with the criteria of adjusted P < 0.1 and an absolute value of log2[fold change] > 1. Differentially accessible peaks were further annotated by HOMER (v.4.10.4)95, the associated motif enrichment analysis was performed by HOMER using the default settings.

Analysis of senescence-induced changes in promoter chromatin accessibility

An MA plot (log2-transformed fold change versus mean average) was used to visualize changes in chromatin accessibility for all peaks. As a peak score, we used an average of TPM-normalized read counts: (1) reads per kilobase were calculated by division of the read counts by the length of each peak in kilobases; (2) the per million scaling factor was calculated as a sum of all reads per kilobase for each sample; (3) reads per kilobase were divided by the per million scaling factor; (4) peaks with the ‘promoter-TSS’ annotation TSS ± 1kb were selected and the average was calculated for each group. For MA plots, we included only those peaks with an average normalized signal > 5. The number of peaks with a log2-transformed fold change of >1 or <−1 was calculated. Normalized ATAC-seq signal profiles of proximal promoters were visualized for key genes using the Integrative Genomic Viewer (v.2.8.13)96.

Transcription factor analysis and activity prediction

For the analysis of transcription regulation, we combined the results of several methods: (1) motif enrichment analysis of differentially expressed genes with the TRANSFAC_and_JASPAR_PWMs and ENCODE_and_ChEA_Consensus_TFs_from_ChIP-X libraries using the R package EnrichR (v.2.1)97; (2) upstream regulator analysis of differentially expressed genes using the commercial Ingenuity Pathway Analysis (IPA, QIAGEN) software98; (3) analysis of transcription factor differential expression using DESeq2 (v.1.28.1); (4) motif enrichment analysis of differentially accessible regions using HOMER (v.4.10.4).

Potential regulators from EnrichR and IPA results passing the threshold of P < 0.05 were used to build a union set of transcription factors, which was further filtered to retain only the molecules with DESeq2 baseMean value > 0. For further validation of the activity status, transcription factors were matched to the known HOMER motifs passing the Benjamini Q < 0.05 threshold.

A discrete scoring scale (inhibited, possibly inhibited, unknown/contradictory, possibly activated, activated) was used to evaluate transcription factor activity based on combined evidence from the EnrichR, IPA, DESeq2 and HOMER results. We used z-score statistics to define the activity status of transcription factors from the EnrichR analysis results by matching the differential expression of target genes with activatory and inhibitory interactions from the Bioconductor package DoRothEA (v.1.0.0)99 and the web-based TRRUST v.2 database100. To define the activity status of transcription factors from IPA upstream regulators analysis results, IPA-calculated z-score and analysis bias was taken into account. Activity predictions were further corrected by differential expression of transcription factors using DESeq2. The expression z-score statistical value was calculated to functionally classify transcription factors as activators or repressors on the basis of the proportion of upregulated and downregulated target genes. We further calculated the chromatin accessibility z-score to estimate the prevalence of HOMER motif enrichment in open versus closed regions that together with the predicted transcription factor function enabled us to validate the RNA-seq activity predictions using ATAC-seq data.

To estimate the level of confidence, for each enrichment result, we calculated a discrete ‘trust’ score, with each point assigned for: (1) EnrichR adjusted P < 0.05; (2) IPA P < 0.05; (3) activity status ‘activated’ or ‘inhibited’; (4) unidirectional absolute z-scores of >2 from both the EnrichR and IPA results; (5) concordance between transcription factor differential expression and the prediction of its activity score; (6) activity validated by the analysis of ATAC-seq data. Transcription factors with average trust > 1 were processed for further analysis.

Functional profiling of transcription factor target gene regulation

For each transcription factor, we merged the target genes from EnrichR and IPA results, split them into upregulated and downregulated and processed them to functional enrichment analysis of canonical pathways (KEGG, Reactome) and GO:BP using R package gprofiler2 (v.0.1.9)101 with the following parameters: correction method ‘FDR’, ‘custom_annotated’ domain score consisting of target genes for all studied transcription factors. Electronic GO annotations were excluded. Gene sets that passed the FDR < 0.05 threshold were processed for further analysis. For GO:BP, we selected the gene sets with a term size of >15 and <500 genes. Transcription factors were further mapped based on the matching terms from the gprofiler2 results to the main functional clusters of the gene sets created previously in GSEA/Cytoscape analysis.

Transcription factors mapped to the same functional cluster in ≥8 (out of 12) Sen versus NSen comparisons were processed for further filtering. We scored as 1 point in each case when any of the following attributes had a value above the upper quartile for a given cluster: number of comparisons, percentage of GSEA terms among all terms with enrichment, −log10 of the average minimum FDR and average trust score. Moreover, we scored as 1 point if the transcription factor was associated with senescence in literature. For graphical representation, we selected examples of transcription factors and target genes based on literature research: 19 transcription factors (out of 29 with a score of ≥2) mapped to 9 clusters (matrix remodelling/fibrosis, interferon signalling, chemotaxis, lipid uptake, IGF regulation, detoxification, gene expression and protein translation, cell cycle, and DNA repair).

Functional profiling of transcriptional regulation of SASP

For each transcription factor upregulated, target genes from the EnrichR and IPA results were merged and intersected with the list of SASP genes. For SASP genes, we extracted GO:MF terms, clustered them into 12 categories (adhesion molecule, chemokine, complement component, cytokine, enzyme, enzyme regulator, extracellular matrix constituent, growth factor, hormone, ligand, proteinase and receptor) and estimated the enrichment of GO:MF clusters with a hypergeometric test using the R function phyper. Correction for multiple comparisons was performed using the Benjamini–Hochberg procedure.

Transcription factors that had target enrichment in the same GO:MF cluster with P < 0.05 in ≥8 (out of 12) Sen versus NSen comparisons were processed for further filtering. We scored 1 point in each case in which any of the following attributes had a value above the upper quartile for a given cluster: the percentage of secreted proteins among targets, the number of comparisons with P < 0.05, the number of comparisons with adjusted P < 0.05, −log10 of the average P value, the average trust score. Moreover, we used ATAC-seq data analysis to score 1 point in cases in which the transcription factor motif was present in the promoter region of at least one SASP gene within the cluster. For graphical representation, we selected 17 transcription factors with a score of ≥2 and with ≥3 comparisons with adjusted P < 0.05. They were associated with five GO:MF categories (extracellular matrix constituent, cytokine, chemokine, complement component and growth factor), for which we selected the most common target genes.

Analysis of lipid metabolism gene set

For the analysis of lipid metabolism, we constructed a gene set using data from multiple sources: KEGG pathway maps (fatty acid degradation, cholesterol metabolism, regulation of lipolysis in adipocytes), WikiPathways (fatty acid oxidation, fatty acid beta oxidation, mitochondrial LC-fatty acid beta-oxidation, fatty acid omega oxidation, fatty acid biosynthesis, triacylglyceride synthesis, sphingolipid metabolism (general overview), sphingolipid metabolism (integrated pathway), cholesterol metabolism (includes both Bloch and Kandutsch–Russell pathways) and cholesterol biosynthesis) and literature research102,103,104. We further estimated the expression of these genes by filtering DESeq2 results (adjusted P < 0.05 in at least 3 out of 12 comparisons) and extracted log2-transformed fold change values to plot the difference in expression between senescent and non-senescent cells.

Reconstruction of ligand–receptor mediated cell–cell communication networks

For reconstructing cell–cell communication networks, we modified the single-cell-based method, FunRes, to account for bulk gene expression profiles39. In brief, transcription factors with an expression value of more than 1 TPM were considered to be expressed. Receptors regulating these transcription factors were detected using a Markov chain model of signal transduction to detect high-probability intermediate signalling molecules105. Ligand–receptor interactions between two cell populations were reconstructed if (1) the receptor is expressed and regulates any transcription factor, (2) the ligand is expressed and (3) the receptor–ligand interaction is contained in the cell–cell interaction scaffold. Finally, a score is assigned to every interaction by multiplying the average receptor and ligand expression in their respective cell populations. Significance was assessed by permuting cell population labels 100 times and recomputing the interaction scores in the permuted datasets. Interactions were considered to be significant if they were at least 2 s.d. greater than the mean of the permuted interaction scores. Only significant interactions were retained in the final network.

Downstream analysis of senescence-induced ligand–receptor interactions

For the functional profiling, we selected ligand–receptor interactions between three senescent cell populations (SCs, FAPs and MCs) and a non-senescent SC population in old mice at 3 d.p.i. We used the Bioconductor package SPIA (v.2.40.0)40 with a reduced set of non-disease KEGG pathway maps to evaluate the activity of a pathway’s downstream ligand–receptor interactions. For each interaction, differentially expressed target transcription factors in non-senescent SCs were split into upregulated and downregulated in comparison to senescent SCs. As a reference set of genes, we took a list of target transcription factors from all of the interactions studied. SPIA analysis was performed with 2,000 permutations, and pPERT and pNDE were combined using the Fisher’s product method. Pathways passing the pGFdr < 0.05 threshold were considered to be significantly enriched. For each pathway, we calculated the ratio of ligand–receptor interactions that activate or inhibit the pathway to the total number of interactions analysed. For results representation, we selected eight activated and eight inhibited pathways with the highest ratio of interactions.

Statistical analysis

The sample size of each experimental group is described in the corresponding figure caption, and all of the experiments were conducted with at least three biological replicates unless otherwise indicated. GraphPad Prism was used for all statistical analyses except for sequencing-data analysis. Quantitative data displayed as histograms are expressed as mean ± s.e.m. (represented as error bars). Results from each group were averaged and used to calculate descriptive statistics. Mann–Whitney U-tests (independent samples, two-tailed) were used for comparisons between groups unless otherwise indicated. P < 0.05 was considered to be statistically significant. Experiments were not randomized.

Reporting summary

Further information on research design is available in the Nature Portfolio Reporting Summary linked to this article.

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National Geographic’s new ‘Stargazer’s Atlas’ is a breathtaking guide to the cosmos (exclusive)

Those seeking out an ideal gift for the astronomy lover in your life need look no further than the sizable heft and heavenly imagery of “Stargazer’s Atlas: The Ultimate Guide to the Night Sky.” (opens in new tab)

Created by an ensemble team of National Geographic experts alongside the orchestration efforts of Andrew Fazekas, a.k.a. The Night Sky Guy, the gorgeous new coffee-table book is not only a utilitarian guide to the heavens, but also a treasure trove of 170 detailed charts, historical photos, space mission images and mind-boggling maps of the planets and moons of our solar system.

This oversized, 432-page hardcover tips the scales at 6 pounds (2.7 kilograms) and is packed with glossy photographs and informative explanations that lure you out into the chilly nocturnal air to gaze up in awe at the cosmos.

Related: Best space books for 2022



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Atlas V rocket launches 2 communications satellites to orbit

An Atlas V rocket lifted off Tuesday evening (Oct. 4) from Florida’s Space Coast, carrying two commercial communications satellites to orbit.

The Atlas V, topped with the twin SES-20 and SES-21 spacecraft, launched Tuesday at 5:36 p.m. EDT (2136 GMT) from Cape Canaveral Space Force Station.

The 196-foot-tall (60 meters) rocket hit all of its marks early. It jettisoned its three solid rocket boosters about 2 minutes after liftoff as planned, for example, and discarded its payload fairing, which protected the two satellites during launch, about 1.5 minutes later. And the Atlas V’s two stages separated at about T+4.5 minutes.

Related: The history of rockets

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But there’s quite a bit of work left to do, for the rocket’s Centaur upper stage still needs to power itself to the deployment destinations for SES-20 and SES-21 — near-circular, near-geosynchronous orbits high above Earth. 

If all goes according to plan, SES-20 will be deployed about 5 hours and 40 minutes after liftoff, and SES-21 will follow suit roughly 40 minutes later. The two spacecraft will then use their onboard propulsion systems to circularize their orbits, which will send them zooming around Earth about 22,300 miles (35,900 kilometers) above the equator, according to a ULA mission description (opens in new tab).

Once the satellites are established in those orbits and have been through a checkout period, SES-20 and SES-21 can begin doing what they were built to do — provide television broadcasting service across the United States for the Luxembourg telecom company SES.

“Built by Boeing with thousands of narrow and steerable beams and the ability to isolate interference sources, the two spacecraft provide SES and future customers the ability to expand, extend or even change a satellite’s coverage area and mission throughout its life,” ULA representatives wrote in the mission description.

“Proven hardware coupled with next-generation technology created an affordable and lightweight spacecraft, enabling two satellites to launch on a single rocket,” they added.

The Atlas V launch is part of a busy week in spaceflight. For example, SpaceX plans to launch the Crew-5 astronaut mission for NASA and another batch of the company’s Starlink internet satellites on two separate missions on Wednesday (Oct. 5), as well as two telecom satellites for the company Intelsat on Thursday (Oct. 6).

Three other missions are on tap for Thursday (Oct. 6) as well, including a Rocket Lab launch that will send to orbit a satellite built by the energy and technology firm General Atomics. 

Editor’s note: This story was updated at 6:15 p.m. EDT on Oct. 4 with news of successful liftoff.

Mike Wall is the author of “Out There (opens in new tab)” (Grand Central Publishing, 2018; illustrated by Karl Tate), a book about the search for alien life. Follow him on Twitter @michaeldwall (opens in new tab). Follow us on Twitter @Spacedotcom (opens in new tab) or on Facebook (opens in new tab).  



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Atlas 5 rocket lifts off from Cape Canaveral at dawn – Spaceflight Now

Live coverage of the countdown and launch of a United Launch Alliance Atlas 5 rocket from pad 41 at Cape Canaveral Space Force Station in Florida. The mission will launch the U.S. Space Force’s SBIRS GEO 6 missile warning satellite toward geosynchronous orbit. Text updates will appear automatically below. Follow us on Twitter.

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United Launch Alliance’s fifth mission of the year lifted off from Cape Canaveral at 6:29 a.m. EDT (1029 GMT) Thursday. An Atlas 5 rocket launched on a $1.2 billion mission with a U.S. Space Force missile warning satellite.

The countdown began at 11:09 p.m. EDT Wednesday (0309 GMT Thursday) with the power-up of the rocket, checks of the launcher’s guidance system, and preparations to start loading cryogenic propellants into the Atlas 5.

The mission was the fifth Atlas 5 flight of the year, and the 95th launch of an Atlas 5 rocket overall. After Thursday’s launch, there are 21 Atlas 5s remaining in ULA’s inventory before the rocket is retired. ULA, a 50-50 joint venture between Boeing and Lockheed Martin, is developing the next-generation Vulcan Centaur rocket to replace the Atlas and Delta rocket families.

The payload for Thursday’s mission was SBIRS GEO 6, the final satellite in the Space Force’s Space Based Infrared System. The SBIRS satellites carry infrared sensors to detect heat plumes from missile launches, giving warning of a potential attack to U.S. military forces and government leaders.

Built by Lockheed Martin, the SBIRS GEO 6 satellite weighed about 10,700 pounds (4,850 kilograms) fully fueled for launch.

The first SBIRS payload in an elliptical orbit launched in 2006, and the military launched the first SBIRS satellite into geosynchronous orbit in 2011. The SBIRS program replaced the military’s Defense Support Program, a series of 23 missile warning satellites launched between 1970 and 2007.

One of the infrared cameras on each SBIRS GEO satellite scans across the spacecraft’s coverage area in a U-shaped pattern. With a fleet positioned around the world, the SBIRS satellites and the remaining long-lived DSP satellites provide global coverage to detect missile launches. Another infrared sensor can be aimed at specific regions of interest.

“There’s a staring sensor that can be pointed at and stare at a fixed point,” said Michael Corriea, Lockheed Martin’s vice president overseeing the SBIRS program. “So for example, you can task it to look over China because there was something you maybe wanted to look at in a particular area, or North Korea.

A United Launch Alliance Atlas 5 rocket stands on its launch pad at Cape Canaveral Space Force Station on Wednesday. Credit: Michael Cain / Spaceflight Now / Coldlife Photography

After a few hours of early countdown preparations, ULA’s launch team at Cape Canaveral’s Atlas Spaceflight Operations Center gave the “go” for the start of cryogenic tanking of the Atlas 5 around 4:30 a.m. EDT (0830 GMT).

Nearly 66,000 gallons of liquid hydrogen and liquid oxygen were loaded into the two-stage Atlas 5 rocket. The Centaur upper stage’s Aerojet Rocketdyne RL10 engine burns the hydrogen and oxygen propellant mix, and the Atlas first stage consumes liquid oxygen with 25,000 gallons room-temperature kerosene fuel, which was loaded into the rocket Tuesday, soon after ULA ground crews rolled the Atlas 5 the launch pad from the nearby Vertical Integration Facility.

Two built-in holds occurred in the countdown, one at T-minus 2 hours and another at T-minus 4 minutes, before the final four-minute terminal countdown sequence to prepare the Atlas 5 rocket liftoff.

The rocket’s propellant tanks were pressurized, and the RD-180 engine ignited at T-minus 2.7 seconds. After building up thrust on the main engine, the Atlas 5 sent the command to light two Northrop Grumman strap-on solid rocket boosters to power the launcher off pad 41 with 1.6 million pounds of thrust.

The version of the Atlas 5 used on the SBIRS GEO 6 mission is known as the “421” configuration, with the first number denoting the size of the payload fairing, the second number representing the number of solid rocket boosters, and the third digit the number of engines on the Centaur stage.

The SBIRS GEO 6 mission marked the ninth and final flight of an Atlas 5 rocket in the 421 vehicle configuration, and the final launch from Cape Canaveral of an Atlas 5 rocket with the Atlas program’s classic conical 4-meter (13-foot) diameter nose cone. One more Atlas 5 with a 4-meter fairing is scheduled to launch later this year from California, while the rest will fly with the larger, more bulbous 5-meter payload fairing.

After liftoff, the 194-foot-tall (59-meter) Atlas 5 rocket, designated AV-097 for this mission, headed east from Cape Canaveral to target the mission’s elliptical, or oval-shaped, geosynchronous transfer orbit

The Atlas 5 surpassed the speed of sound in 49 seconds, then shed its spent strap-on boosters at T+plus 2 minutes, 13 seconds.

The first stage’s RD-180 engine fired until T+plus 4 minutes, 12 seconds. Six seconds later, the first stage separated from the Atlas 5’s Centaur upper stage, which ignited its RL10 engine at T+plus 4 minutes, 28 seconds. The clamshell-like payload shroud on top of the Atlas 5 jettisoned at T+plus 4 minutes, 36 seconds, once the rocket was flying above the thick lower layers of the atmosphere.

Three RL10 engine burns are planned before the Atlas 5 releases the SBIRS GEO 6 satellite at T+plus 3 hours, 1 minute.

The Atlas 5’s guidance computer will aim to release the spacecraft in an orbit ranging in altitude between 3,242 miles (5,218 kilometers) and 21,956 miles (35,335 kilometers), with an inclination angle of 17.63 degrees to the equator.

This cutaway graphic shows the Atlas 5 rocket’s “421” variant used to launch the SBIRS GEO 6 satellite. Credit: United Launch Alliance

The SBIRS GEO 6 spacecraft will use an on-board propulsion system to steer itself to a circular geosynchronous orbit that is continuously at an altitude of nearly 22,300 miles over the equator. In that orbit, the satellite’s velocity will be fixed with the rate of Earth’s rotation, giving the craft’s infrared early warning sensors a constant view of the same part of the planet.

The satellite will also extend power-generating polar panels and light shades to begin fine-tuning the performance of is heat-seeking sensors.

SBIRS GEO 6 should be ready to enter operational service in early 2023, according to Space Force officials. The satellite is designed for a 12-year mission. Read our mission preview story for more details on SBIRS GEO 6.

ROCKET: Atlas 5 (AV-097)

MISSION: SBIRS GEO 6

PAYLOAD: SBIRS GEO 6 missile warning satellite

CUSTOMER: U.S. Space Force

LAUNCH SITE: SLC-41, Cape Canaveral Space Force Station, Florida

LAUNCH DATE: Aug. 4, 2022

LAUNCH WINDOW: 6:29-7:09 a.m. EDT (1029-1109 GMT)

WEATHER FORECAST: 80% chance of acceptable weather

BOOSTER RECOVERY: None

LAUNCH AZIMUTH: East

TARGET ORBIT: Perigee of 3,242 miles (5,218 kilometers); Apogee of 21,956 miles (35,335 kilometers); Inclination angle of 17.63 degrees to the equator.

LAUNCH TIMELINE:

  • T-00:00:02.7: RD-180 ignition
  • T+00:00:01.1: Liftoff
  • T+00:00:06.0: Begin pitch/yaw maneuver
  • T+00:00:48.9: Mach 1
  • T+00:00:52.5: Maximum aerodynamic pressure (Max-Q)
  • T+00:02:13.3: Solid rocket booster jettison
  • T+00:04:12.4: Atlas booster engine cutoff (BECO)
  • T+00:04:18.4: Atlas/Centaur stage separation
  • T+00:04:28.4: Centaur first main engine start (MES-1)
  • T+00:04:36.4: Payload fairing jettison
  • T+00:12:55.4: Centaur first main engine cutoff (MECO-1)
  • T+00:22:54.6: Centaur second main engine start (MES-2)
  • T+00:27:38.8: Centaur second main engine cutoff (MECO-2)
  • T+02:57:40.5: Centaur third main engine start (MES-3)
  • T+02:58:38.4: Centaur third main engine cutoff (MECO-3)
  • T+03:01:27.4: SBIRS GEO 6 spacecraft separation

MISSION STATS:

  • 677th launch for Atlas program since 1957
  • 378th Atlas launch from Cape Canaveral
  • 266th mission of a Centaur upper stage
  • 243rd use of Centaur by an Atlas rocket
  • 513th production RL10 engine to be launched
  • 2nd RL10C-1-1 engine launched
  • 101st flight of an RD-180 main engine
  • 95th launch of an Atlas 5 since 2002
  • 37th U.S. Air Force/Space Force use of an Atlas 5
  • 18th-19th GEM-63 solid rocket boosters flown
  • 79th launch of an Atlas 5 from Cape Canaveral
  • 5th Atlas 5 launch of 2022
  • 137th Evolved Expendable Launch Vehicle flight
  • 152nd United Launch Alliance flight overall
  • 87th Atlas 5 under United Launch Alliance
  • 110th United Launch Alliance flight from Cape Canaveral
  • 6th launch of a SBIRS GEO satellite
  • 57th 400-series flight of the Atlas 5
  • 9th Atlas 5 to fly in the 421 configuration
  • 106th launch from Complex 41
  • 79th Atlas 5 to use Complex 41
  • 33rd orbital launch overall from Cape Canaveral in 2022



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ULA’s Atlas 5 launches U.S. Space Force experimental missile-warning satellite

The $1.1 billion USSF-12 mission flew to geosynchronous Earth orbit

WASHINGTON — A United Launch Alliance Atlas 5 rocket on July 1 launched the USSF-12 mission for the U.S. Space Force. The rocket lifted off at 7:15 p.m. Eastern from Space Launch Complex-41 at Cape Canaveral Space Force Station, Florida.

The $1.1 billion USSF-12 mission to geosynchronous Earth orbit carried two satellites: the Wide Field of View (WFOV) missile-warning spacecraft for the U.S. Space Force, and a ring-shaped payload adapter with six classified smallsat experiments for DoD’s Space Test Program.

This was the 94th mission of the Atlas 5 rocket. The vehicle’s first stage was powered by an RD-180 engine and four solid rocket boosters, and the Centaur upper stage by an Aerojet Rocketdyne RL10C-1 engine. To encapsulate the satellites, ULA used a 5.4-meter diameter payload fairing made by Beyond Gravity (formerly RUAG Space).

USSF-12 was originally scheduled to fly in April but was delayed for undisclosed reasons. A June 30 launch attempt was scrubbed due to bad weather conditions

WFOV is a mid-sized spacecraft made  by Millennium Space Systems with an infrared sensor payload developed by L3Harris Technologies under a 2016 contract from the U.S. Air Force. WFOV is a testbed satellite, meaning that it is not part of an operational missile-warning constellation but a stand-alone experiment.

At 1,000 kilograms, WFOV is about one-fourth the size of the Space Based Infrared System (SBIRS) spacecraft that currently perform strategic and tactical missile warning for the Defense Department. ULA will launch the SBIRS-6 satellite in late July.

The WFOV satellite, equipped with a staring sensor, will be used to test different ways to collect and report missile launch data. The Space Force said the research will inform the design of future missile-warning satellites. WFOV will be able to continuously monitor up to one-third of the Earth’s surface.

The ring-shaped smallsat carrier payload, known as a propulsive ESPA ring, was built by Northrop Grumman.

Both satellites on USSF-12 are scheduled to reach orbit six hours after liftoff,  a trajectory requiring three Centaur engine burns. ULA used an in-flight power system to keep the WFOV satellite’s batteries topped off throughout the six-hour flight to geosynchronous orbit.

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Atlas V rocket launches hypersonic-missile-tracking craft for US military

A missile-warning satellite and another spacecraft are on their way to orbit to help the U.S. military get better at tracking fast-moving threats.

The two U.S. military surveillance satellites lifted off today (July 1) atop a United Launch Alliance (ULA) Atlas V rocket, which rose off a pad at Florida’s Cape Canaveral Space Force Station at 7:15 p.m. EDT (2315 GMT) on a mission for the U.S. Space Force called USSF-12.

The Atlas V’s first and second stages separated four and a half minutes after liftoff, a milestone that was soon followed by a more than six-minute burn of the upper-stage Centaur’s engine. After two more Centaur burns, the two satellites will be ready to be deployed into geosynchronous orbit, about 22,300 miles (35,900 kilometers) above Earth. But that won’t happen until about six hours after liftoff.

Related: The most dangerous space weapons ever

(Image credit: ULA)

One of the two spacecraft, called the Wide Field of View (WFOV) satellite, is the Space Force Space System Command’s (SSC) testing platform for a new generation of missile-surveillance technology. The other is a satellite bus hosting a number of technology demonstrations for the U.S. Department of Defense (DoD). It is called, simply, the USSF-12 Ring.

Both WFOV and the USSF-12 Ring are considered classified payloads in support of national security, so not much information is available for either of them. However, government agency and contractor representatives were able to provide some details during a call with reporters on Tuesday (June 28).

The USSF-12 Ring was built by Northrop Grumman based on the aerospace company’s ESPAStar product line. This ring is being flown for the DoD and features six unique payload ports as well as an independent propulsion system, Matt Verock, vice president of space security for Northrop Grumman, said during the call. 

The DoD has not disclosed details regarding any of those payloads, but DoD space test program director Lt. Col. Jon Shea said that the USSF-12 Ring and its payloads “will deploy key pathfinders for future capabilities and deliver innovative technologies to help us advance … future missions.”

WFOV has an imaging sensor that’s more than 6 feet tall (about 2 meters). The sensor was built by L3Harris Technologies, a company that also supplied optical components for NASA’s Hubble and James Webb space telescopes, as well as the Nancy Grace Roman space telescope, which is currently in development. The sensor was designed for a new type of weapons detection system — the tracking of hypersonic weapons — and WFOV will help SSC calibrate its accuracy. 

Russian state media announced a successful test of the country’s new hypersonic Kinzhal missile in 2018 and published an animated video of the missile being fired at the United States. The Kinzhal missile is reportedly able to travel five times faster than the speed of sound and capable of striking targets anywhere in the world.

Current space-deployed weapons tracking systems focus on ballistic missiles, which have limited maneuverability. The DoD has created a new system, the Overhead Persistent Infrared program (OPIR), to track next-generation hypersonic threats, such as the Kinzhal. WFOV is the testbed for those technologies. 

“The threat is imminent right now,” Col. Heather Bogstie, senior materiel leader for the SSC’s Resilient Missile Warning, Tracking and Defense Acquisition Delta, said during Tuesday’s call. “[WFOV] is really going to be an important pathfinder for our future MEO [middle Earth orbit] missile track systems.” 

She described the WFOV mission as a “digital engineering demo,” which will give “24/7 coverage across 3,000+ kilometers [1,860 miles] over the Pacific Theater.” 

Once the WFOV satellite and the USSF-12 Ring reach their assigned geosynchronous orbits, the two are designed for mission operability for up to three years. WFOV’s successors, the OPIR program satellites, are on track to begin launching as soon as 2025, according to an SSC release, with a total of five slated to launch between then and 2028.

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Countdown begins for Atlas 5 launch from Cape Canaveral – Spaceflight Now

Live coverage of the countdown and launch of a United Launch Alliance Atlas 5 rocket from pad 41 at Cape Canaveral Space Force Station in Florida. The mission, known as USSF 12, will launch the U.S. Space Force’s Wide Field of View Testbed satellite and the USSF 12 Ring spacecraft into geosynchronous orbit. Text updates will appear automatically below. Follow us on Twitter.

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A United Launch Alliance Atlas 5 rocket is ready to boost two experimental U.S. Space Force satellites all the way to geosynchronous orbit in a six-hour mission launching from Cape Canaveral Thursday. The two-hour launch window opens at 6 p.m. EDT (2200 GMT).

There is a 40% chance of favorable weather at the opening of the window Thursday in the official launch forecast issued by the Space Force’s 45th Weather Squadron. The forecast improves later in the window, when there’s a 60% chance of favorable conditions for launch.

The mission, codenamed USSF 12, will be the fourth Atlas 5 flight of the year, and the 94th launch of an Atlas 5 rocket overall. It is one of 23 Atlas 5s remaining in ULA’s inventory before the rocket is retired. ULA, a 50-50 joint venture between Boeing and Lockheed Martin, is developing the next-generation Vulcan Centaur rocket to replace the Atlas and Delta rocket families.

One of the payloads on the mission is the Space Force’s Wide Field Of View, or WFOV, Testbed satellite to demonstrate a new infrared sensor capable of detecting and tracking missile launches, providing early warning of a potential attack on the United States of allied nations.

The WFOV spacecraft will ride to space in the upper portion of the Atlas 5 rocket’s payload compartment. A secondary payload, called the USSF 12 Ring, is positioned below the WFOV spacecraft for launch. It hosts multiple payloads, experiments and prototypes, but details about their missions are classified.

A Space Force spokesperson told Spaceflight Now the entire USSF 12 mission, including the payloads and launch services, cost about $1.1 billion.

ULA’s Atlas 5 rocket on the launch pad before the USSF 12 mission. Credit: United Launch Alliance

The countdown for the launch Thursday began at 10:40 a.m. EDT (1440 GMT). ULA teams planned to turn on the Atlas 5 flight computer, complete checks of the rocket’s guidance system, and then configure the vehicle for the start of cryogenic tanking around 4 p.m. EDT (2000 GMT).

Nearly 66,000 gallons of liquid hydrogen and liquid oxygen will be loaded into the two-stage Atlas 5 rocket. The Centaur upper stage’s Aerojet Rocketdyne RL10 engine burns the hydrogen and oxygen propellant mix, and the Atlas first stage consumes liquid oxygen with 25,000 gallons room-temperature kerosene fuel, which was loaded into the rocket Wednesday, soon after ULA ground crews rolled the Atlas 5 the launch pad from the nearby Vertical Integration Facility.

Two built-in holds are planned in the countdown, one at T-minus 2 hours and another at T-minus 4 minutes, before the final four-minute terminal countdown sequence to prepare the Atlas 5 rocket liftoff.

The rocket’s propellant tanks will be pressurized, and the RD-180 engine will ignite at T-minus 1 second. After building up thrust on the main engine, the Atlas 5 will send the command to light four Northrop Grumman strap-on solid rocket boosters to power the launcher off pad 41 with 2.3 million pounds of thrust.

The version of the Atlas 5 launching on the USSF 12 mission is known as the “541” configuration, with the first number denoting the size of the payload fairing, the second number representing the number of solid rocket booster, and the third digit the number of engines on the Centaur stage.

The 196-foot-tall (59.7-meter) Atlas 5 rocket, designated AV-094 for this mission, will head east from Cape Canaveral to target the mission’s equatorial orbit more than 22,000 miles (nearly 36,000 kilometers) above Earth.

The Atlas 5 will surpass the speed of sound in 58 seconds, then shed its spent strap-on boosters at T+plus 1 minute, 48 seconds. The 5.4-meter-wide (17.7-foot) composite payload shroud will jettison at T+plus 3 minutes, 25 seconds, and the Russian-made RD-180 core stage engine will fire until T+plus 4 minutes, 24 seconds.

This graphic illustrates the components of the Atlas 5 rocket for the USSF 12 mission. Credit: United Launch Alliance

The USSF 12 mission marks the 100th flight of an RD-180 engine since it first launched in May 2000 on an Atlas 3 rocket.

After separation of the Atlas first stage, ULA’s Centaur upper stage will take over the flight with three burns of its single RL10 engine to first place the two Space Force payloads into a parking orbit, then propel the mission into higher orbits and on a trajectory hugging the equator.

The WFOV Testbed spacecraft, built by Millennium Space Systems, will separate from the Centaur upper stage at T+plus 5 hours, 49 minutes. An adapter structure will release about 10 minutes later, revealing the Northrop Grumman-built USSF 12 Ring payload for separation at T+plus 6 hours, 5 minutes.

ROCKET: Atlas 5 (AV-094)

MISSION: USSF 12

PAYLOAD: WFOV Testbed and USSF 12 Ring

LAUNCH SITE: SLC-41, Cape Canaveral Space Force Station, Florida

LAUNCH DATE: June 30 , 2022

LAUNCH WINDOW: 6:00-8:00 p.m. EDT (2200-0000 GMT)

WEATHER FORECAST: 60% chance of acceptable weather

BOOSTER RECOVERY: None

LAUNCH AZIMUTH: East

TARGET ORBIT: Approximately 22,440 miles, 0.0 degrees inclination

LAUNCH TIMELINE:

  • T-00:00:01.0: RD-180 ignition
  • T+00:00:01.0: Liftoff
  • T+00:00:06.9: Begin pitch/yaw maneuver
  • T+00:00:57.8: Mach 1
  • T+00:01:07.4: Maximum aerodynamic pressure (Max-Q)
  • T+00:01:48.4: Solid rocket booster jettison
  • T+00:03:25.6: Payload fairing jettison
  • T+00:04:24.3: Atlas booster engine cutoff (BECO)
  • T+00:04:30.3: Atlas/Centaur stage separation
  • T+00:04:40.2: Centaur first main engine start (MES-1)
  • T+00:10:58.2: Centaur first main engine cutoff (MECO-1)
  • T+00:23:13.6: Centaur second main engine start (MES-2)
  • T+00:28:41.9: Centaur second main engine cutoff (MECO-2)
  • T+05:43:54.1: Centaur third main engine start (MES-3)
  • T+05:46:20.0: Centaur third main engine cutoff (MECO-3)
  • T+05:49:36.0: WFOV Testbed spacecraft separation
  • T+05:59:03.9: Booster adapter separation
  • T+06:05:21.0: USSF 12 Ring spacecraft separation

MISSION STATS:

  • 676th launch for Atlas program since 1957
  • 377th Atlas launch from Cape Canaveral
  • 265th mission of a Centaur upper stage
  • 242nd use of Centaur by an Atlas rocket
  • 512th production RL10 engine to be launched
  • 40th RL10C-1 engine launched
  • 100th flight of an RD-180 main engine
  • 94th launch of an Atlas 5 since 2002
  • 36th U.S. Air Force/Space Force use of an Atlas 5
  • 14th-17th GEM-63 solid rocket boosters flown
  • 78th launch of an Atlas 5 from Cape Canaveral
  • 4th Atlas 5 launch of 2022
  • 136th Evolved Expendable Launch Vehicle flight
  • 151st United Launch Alliance flight overall
  • 86th Atlas 5 under United Launch Alliance
  • 109th United Launch Alliance flight from Cape Canaveral
  • 35th 500-series flight of the Atlas 5
  • 9th Atlas 5 to fly in the 541 configuration
  • 105th launch from Complex 41
  • 78th Atlas 5 to use Complex 41
  • 28th orbital launch overall from Cape Canaveral in 2022



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