Rideshare/Multi Manifest Payload Overview - NASA
Rideshare/Multi‐Manifest PayloadOverviewBob Caffreyrobert.t.caffrey@nasa.gov, 301‐286‐0846June 2019STP‐1–30’ tall x 27.6’ diaAir ForceNASA / EELVNASA / SLSCommercial
Rideshare Poster‐child: DSCOVR & TESSDSCOVR: Feb 2015TESS: April 20182500 kg of unused mass went to L‐1 300kg S/C and 3000 kg excess on a TLI orbit6/13/20192
Government Rideshare: Past, Present & FuturePast Missions (DSCOVR)6/13/2019Present Missions (STP‐2)Future Missions (PACE?)3
NASA Competitive ao/pdf 2020190403‐final.pdf)NASA Science Opportunity6/13/2019PlannedAO RequiredAO Release Date Launch WindowAstrophysics Explorers MOO3‐MAR‐2019AO 6.5 yearsAstrophysics SMEX3‐Apr‐2019AO 6.5 yearsDiscovery AO1‐Apr‐2020AO 6.5 yearsHeliophysics MIDEX AOQ3 FY 2019AO 6.5 yearsEarth Venture Mission‐3 AOQ4 FY 2019AO 6.5 yearsEarth Venture Ins‐6 AOQ3 FY 2020AO 6.5 yearsAstrophysics MIDEX & MOOQ4 FY 2021AO 6.5 years4
Multi‐Manifest Payload Launch Options(Exploring each option’s cost, schedule, risk, & performance)RideshareOptions?NASA RideshareD4USAF/DoD RSCommercial RSRideshare orHosted P/L?D2Hosted P/LOptions?NoDedicatedLaunch?PayloadNASA HPD5USAF/DoD HPCommercial HPD1YesSmall L/V?D36/13/2019Vendor aaaoooVendor zzz5
NASA & Air Force Rideshare Options(Key: Air Force Missions (bold) & NASA Missions (non‐bold)Year2019LEO(mid inc)STP‐2RALI ( 3)LEO(hi EUSAFUSAFPSYCHEUSAFUSAFUSAF (3 )EM‐2USAFUSAF (2 )GOES‐UUSAFUSAF (3 ea)USAFUSAF (3 )2023STP‐S292024202520266/13/2019MEOOther/ TLIJPSS‐3USAFSentinel‐6bLandsat‐10IMAPNew Front‐4EM‐3GDCEM‐4Discovery 15EM‐56
USAF Rideshare Example: STP‐2(A five burn mission delivering multiple payloads into several different orbits)February 6th, 2018Spring/Summer 2019STP‐2: multiple payloads, multiple orbits‐Orbit 1: 300 x 720 km at 28.4 deg inc., 1 8 deployed‐Orbit 2: 720 x 720 km at 24 deg inc., 11 deployed‐Orbit 3: 6000 x 12000 km at 45 deg, 1 deployed6/13/20197
USAF Rideshare & Hosted Payload Example:OTB‐1 on STP‐2 An orbital test bed for experimentation and demonstrationof payloads, subsystems, and equipment– OTB hosted payloads NASA JPL Deep Space Atomic Clock USAFA iMESA‐R: sampling of electrostatic field, electron density,plasma irregularities AFRL/Vanguard MSA: modular solar panels TUI terminator tape deorbit device: validation of augmentedcubesat tether OTB payload suite: evaluation, demonstration, heritageo FlexRX: programmable receivero RadMon: radiation effects monitoro CUSP: University of Colorado collaboration, off‐the‐shelfcomponentso High‐efficiency solar cell experiment: performancecharacterizationo Electronic Test Bed: new electronic components, processors, andmemory devices6/13/20198
NASA Rideshare Example: ESPA on Landsat‐9(A four burn mission delivering rideshare payloads to a 550km SSO orbit)USAF and NASA Payloads on theLandsat‐9 Mission (Atlas‐V)Landsat 9 withan ESPA Ring6/13/20199
Notional Commercial Rideshare Opportunities(contact vendors for details, vendor provided quad charts in backup)YearLEO(Low Inc.)Polar(Hi Inc.)2018NR, TS, TVSF, TS, TV2019SF, TV, NRSF, TS, TV2020SF, TV, NRGEOSF, NR,TV, MXSF, NR,TVSF, TV (GTO),TV (EE)SF, TVSF, TVSF, TV (GTO)2021SF, TV,NR, MXSF, TV, MXSF, TVSF, TV (GTO)2022TV, NRSF, TVSF, TVSF, TV (GTO)2023TV, NRSF, TVSF, TVSF, TV (GTO)SF ‐ SpaceFlightMX – Maxar (Loral)6/13/2019TS ‐ TriSeptNR ‐ NanoRacksOtherSF, TV (GTO)TV ‐ TyvcakNote: This data is the result of a market survey and not an endorsement10
Commercial Rideshare Example:SpaceFlight SSO‐A6/13/201911
Past and Future LaunchMetrics Spacecraft launched: 224– Mass ranging from 1U’s to 900kg– 19 Missions to LEO, GTO (Lunar), & GSO 17 Missions scheduled for 2019 USG Customers:– NASA: ARC, JPL– DoD: AF Space Test Program, ORS Office,AF Academy, AF Research Laboratory, USSOCOM, DHS, Intel, SPAWAR, DARPAPercent 15.50%InternationalDedicated RideshareMission F9 (SSOA): Dec 18Most spacecraft on singlemission: 64 s/c, 18 countries,& 35 customers represented Spaceflight has another 70 spacecraftmanifested ranging from 1U to 1250kgGTO/GSO Rideshare: Feb 19 Launch Vehicle and hardware agnostic– Established agreements with current andnew entrant providers6/13/2019Space IL: Lunar MissionUSG: GSO Mission12
Commercial Rideshare Example: NGC ESPAStar6/13/201913
Rideshare ESPA Spacecraft OptionsDefined by USAF RUG & ESPA Users GuideRideshare CarrierMax entsABC80kg34"x20"x20" 8/15" cir.ESPA (1 of 6 ports)257kgESPA Heavy (1 of 6 ports)450kg8/15" cir.24"x28"x38"& 15" squ.ESPA Grande (1 ‐ 4 ports)700kgESPA Grande Heavy (1‐4)700kg42"x46"x56" 15/24" cir.42"x46"x38" & 24" squ.Aquila (A‐Deck) 1,00056‐diax60"h 24/38" cir.Aquila (dual‐P/L adaptor) qualifiedPropulsive ESPA S/C 2,8004m‐diax24"h62" diaPorts for Rideshare P/L or Hosted P/LPropulsive ESPA Grande 4,4005m‐diax42"h62" diaPorts for Rideshare P/L or Hosted P/LESPA Grande6/13/2019APC Operational1/4"ESPA Operational5/16"1/4"ESPA Grande Operational(5m and 4m faring)5/16"A‐Deck / AquilaPropulsive ESPA14
Rideshare Spacecraft OptionsRideshare Spacecraft (RSC) Decision TreeVendor A:Cost:Risk:Benefits:Vendor B:Cost:Risk:Benefits:S/CVendor?D5oooVendor X:6/13/2019Cost:Risk:Benefits:Capturing the cost, risk, and benefits of the rideshare spacecraft options15
Commercial Rideshare Spacecraft Options(contact vendors for details, vendor provided quad charts in backup)RideshareAdaptor/CarrierBall AerospaceBoeing/ SMSGA(Surrey US)SSTL‐150ESPAESPA Class S/CBCP SmallBoeing/502XSESPA Grande Class S/CBCP SmallBoeing/502SSSTL‐300A‐Deck Class S/CBCP LargeBoeing/502MSSTL‐600Propulsive ESPA S/CBCP Small‐‐‐SSTL‐600Propulsive ESPA GrandeBCP Large‐‐‐SSTL‐600MillenniumSpace OV(AQUILA M8)WFOV(AQUILA M8)Millennium/OMSMoogSpace & Def.NGIS(Orbital‐ATK)Sierra NevadaCorp. (SNC)SN‐30L, SN‐30G,& SN‐50LSN‐100L, SN‐200L, & SN‐200G‐‐‐NGIS ESPASat‐‐‐NGIS N‐1000METEORESPAStar (1)SN‐1000 Note: This data is the result of an open RFI/market survey and not an endorsement6/13/201916
Hosted Payload OptionsNASA HP Opportunities:Cost:Risk:Benefits:USAF/DoD HP Opportunities:Cost:Risk:Benefits:Hosted P/L?D5Commercial HP Opportunities: Cost:Risk:Benefits:Capturing the cost, risk, and benefits of hosted payload implementation options6/13/201917
What is a Hosted Payload (HPL)?A Payload integrated on someone else’s S/CNASA’s GOLD HP on a Commercial BusNASA & USAF HP’s on a Commercial Bus6/13/2019NASA’s Laser HP on a USAF BusNASA’s GeoCarb HP on a Commercial Bus18
Rideshare / ESPA Heritage: Capacity v. Flown the lost opportunity of empty slotsS/CCarrierLaunch Date Capacity FlownESPAMarch 200764Propulsive ESPAJune 200911ESPA Grande (2ea)July 201486ESPA/ANGELSJuly 201461ESPA Grande (3ea) December 20151211ESPAJuly 201660Total:3923S/CMissionSTP-1LCROSSOG2- 1AFSPC-4OG2-2AFSPC-66/13/2019L/VAtlas 5Atlas 5Falcon 9Delta IVFalcon 9Delta IVSTP‐1LCROSSOG2‐2EmptySlots2025161619
CapSat‐Capsulation Satellite: The New GAS CanESPA Class Spacecraft taking advantage of unused launch vehicle mass to orbit Mission Description: Capsulation Satellite or CapSat is a low cost, 3 axisstabilized, modularized and standardized spacecraft,based on using pressurized volumes which allowruggedized COTS hardware to be flown reliably inspace in a manner similar to the NASA Hitchhiker-GetAway Special or GAS Can Program.The Capsulation Satellite Science Instrument Tube orCapSIT is a standardized interface allowing logydemonstrations that can be integrated quickly into thebus.CapSIT is fully qualified for flight independent of theCapSat spacecraft and maybe fully pressurized or notas desired.CapSatCapsulation Satellite6/13/2019–Cutaway viewCapSITCapsulation SatelliteScience Instrument Tube–Top View–Bottom View20
NASA Rideshare Info: S3VI /2019Jointly Sponsored by the Space Technology Mission Directorate (STMD) and theScience Mission Directorate (SMD)21
Backup charts 6/13/201922
Example ESPA ConfigurationsNameESPA P/N# ofPortsØ ofPortsESPAHeightPortPayloadESPAMassNotesStandard ESPA6-15-24615”24”181 kg136 kg¼” BoltsESPA Heavy6-15-24615”24”322 kg136 kg5/16” BoltsEAGLE2-15-24-4PT215”24”181 kg136 kg4x 4 Point Mounts12-11.7-241211.7”24” 85 kg136 kg“1/2 ESPA”4-24-32424”32”320 kg170 kg24” Port Min Height4-24-42-SP424”42”320 kg173 kg¼” Bolts, LightweightESPA Grande4-24-42424”42”320 kg211 kg¼” BoltsGrande Heavy4-24-42424”42”454 kg211 kg5/16” Bolts“SHERPA”5-24-42524”42”320 kg212 kg4-24-48424”48”454 kg238 kg5/16” BoltsLong ESPA4-24-60424”60”320 kg286 kg¼” BoltsLong ESPA4-24-60424”60”454 kg286 kg5/16” Bolts6/13/201923
Secondary Payload AdaptersESPASUMWafer AdaptersESPAFlat Plate AdaptersCASPARFANTM-RiDESmall Launch Adapterand SL-OMV(Ø24” to Ø38”)ESPA n-d-hn number of ports, d port diameter (inches), h ring height (inches)6/13/2019OMV (Ø62”)24
Rideshare Broker Quad‐charts Note: This data is the result of a market survey and not an endorsement6/13/201925
Heritage / Schedule Information: Commercial ISS Satellite Deployments (CubeSats andMicroSats up to 90kg) External Cygnus CubeSat Deployments Above ISS Additional Expendable Launch Vehicle OpportunitiesAvailable (i.e. PSLV) 231 SmallSats deployed to date (19 launches) Quarterly flights to ISS ISS External Platform Hosting on JEM External Facility NanoRacks Bishop Commercial Airlock launching onSpaceX CRS-21 with additional SmallSat deployment andhosted payload capabilitiesCompany Information:Product Information: NanoRacks, LLC –––Established 2009 ( 50 employees)Primary Offices in Houston and Washington, DChttp://nanoracks.com/– Technical: Conor Brown or Henry Martincbrown@nanoracks.com, (703)973-6821hbmartin@nanoracks.com, ((859) 559-7322 Sales: Allen Herbert aherbert@nanoracks.com, (703) 677-4857 Contract Mechanisms6/13/2019 Flexible Commercial Contracting GSA Contract #: 47QRAA18D004R Contracting with NASA Centers and other USG entities viastandardized JSC Services Contract 51.6º inclination, 445-500km circular orbitSmallSat and MicroSat Deployment from PSLV––info@nanoracks.com51.6º inclination, 400-420km SMAUp to 90kg to date (larger capacity available in 2021 uponlaunch of NanoRacks Airlock module to ISS)CubeSat Deployment from Cygnus ISS Ressupply Vehicle– General Inquiries:51.6º inclination, 400-420km circular orbitMicroSat Deployment from ISS–– Point of Contact: CubeSat Deployment from ISSPolar Orbit ( 98º inclination), 450-600kmMid-Inclination Orbit (40-50º inclination), 450-600kmAdditional Brokerage Services for ELVs–Launch brokerage and mission management services fornearly any expendable launch vehicle on the market26
One Stop Integration & Launch Services Spaceflight is a next-generation, integratedspace services and solutions company thatis changing how small satellites are built,launched and operated to improve accessto space and enable persistent globalawareness Business Sectors– Launch & Integration Services– Small Space Systems Development– Integrated Data Analytics Platform Small Business with 155 employeesProducts/Services: Providing Launch Services since 2010 On-line pricing & payment schedules forstandard missions Rideshare/Annual Dedicated RideshareMissions to LEO, GSO, & GTO Experienced staff & in-house integrationfacility to provide– Documentation, ICDs, MA, MSPSP, Masterschedule, shipping, fit‐check– Adapters, Separation Systems, dispensers– 247 payloads launched to date; 150 to come 5-Year: GSA Contract: GS-00F-036DA Other commercial and USG contractsValerie@spaceflight.com: Director of Government BusinessScott@spaceflight.com: Chief Engineer & Sr Mission 191505 Westlake Ave, Ste 600Seattle, WA 98109 USA27
Rideshare Pricing On line pricing and quotes at: www.spaceflight.com USG Contracts:o NASA/Ames: Task Ordering IDIQo NASA/KSC: Cubesat launch and integrationo GSA: Launch and Integration Services On‐boarding more rates to include 150kgs and GTO/GSO6/13/201928
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Tyvak Nano-Satellite Systems Inc.Supporting USGSmallSat Enablers3U P-POD3U Rail-POD6U NLAS12U NLASMicroAMPPOrbital Maneuvering VehicleLaunch Vehicle AvionicsWith MoogNASA ELaNa and CSLILaunch Space PortsArianespace SoyuzArianespace VegaEurockot RockotISRO PSLVKosmotras DneprOrbital Sciences Minotaur COrbital Sciences Minotaur 1Orbital Sciences Minotaur 4Orbital Sciences Taurus XLSpaceX Falcon 1SpaceX Falcon 9ULA Atlas VULA Delta IINASA SLS (in g AFB, USACape Canaveral AFS, USANASA Wallops, USAReagan Test Site, KwajaleinGuiana Space Center, KourouBaikonur Cosmodrome, KZYasny Launch Base, RussiaPlesetsk Cosmodrome, RussiaSatish Dhawan Space Centre, India–––––––––––NASA LSPNASA MSFCNASA JPLNRODoDESAULARocketLabVarious US CommercialVarious US UniversitiesForeignGovt./Comm./Univ.DoD, USAF, NROCompany Information: VP, Commercial Space and LaunchDavid CaponioDavid.Caponio@tyvak.com310-923-3611 15330 Barranca Parkway, Irvine CA, 92618 Formed in 2011, 90 engineers, 35,000 sqft facility includingsecured office and lab space Tyvak provides turnkey launch services from rapid 2 monthcall up from ATP to launch on commercial, DoD, and NASAmissions Launch hardware consisting of dispensers with 80%vibration reduction (6U/12U), to avionics to control a LV, anda maneuverable upper stage partnered with Moog.6/13/2019Flight Heritage with Cal Poly:Tyvak SmallSat Launch Process:Tyvak Responsible ForLaunch Vehicle Focuses OnRequirements andInterface DefinitionLaunchSeparation System &SmallSat Mission SupportPayloads to OrbitHardware CertificationSmallSat IntegrationAcceptance Test/CoFRDelivery to LVAssistance withLV Integration30
Northrop Grumman Rideshare Support6/13/201931
Northrop Grumman:Rideshare Opportunities Antares (with Cygnus):––––CubeSats DeployersPayloads Smaller than ESPA (longer but skinnier), mass flexibleOrbit: 185x300 km, 51.6⁰Antares without Cygnus: ESPA Payloads ‐ shorter than standard ESPA P/L (due to 3.9 M faring v. 4.3 M diameter) Cygnus:– CubeSats Deployers– Payloads less than 50 kg, custom shapes – see quad chart– ISS Orbit: 400 km, 51.6⁰ (post ISS: slightly above/below & different inclination) Launch Opportunities– Antares and Cygnus will launch several times a year through 2022 (3 possiblelaunches in 2017).6/13/201932
Rideshare Spacecraft Quad‐charts Note: This data is the result of a market survey and not an endorsement6/13/201933
Ball Configurable Platform (BCP) For RideshareHeritage / Schedule Information:IXPESPHERExCompany Information: Dr. W D Deininger Dr. J. Weinberg 303.939.5314 303.939.4215 wdeining@ball.com jweinber@ball.com www.ball.com Boulder & Broomfield, Colorado, USA, 4000 employees, Active SmallSat Projects Include: STPSat-2,STPSat-3, GPIM, IXPE, NeoWISE (WISE),SPHEREx6/13/2019 STPSat-2, Launched Nov 2010, 2 payloads STPSat-3, Launched Nov 2013, assembled in 47days, 6 payloads GPIM, planned launch summer 2019, greenpropellant propulsion system prime payload, 3secondary payloads; contract start to spacecraftbus complete – 24 months; Launch June 2019 IXPE, in development, Mission CDR June 2019;launch planned April 2021 SPHEREx, in development, phase B start May2019, launch planned November 2022Small BCP Product Information: Orbit; 400 km to 1200 km Inclination: 0 deg to sun-synchronous Stabilization: 3-axis, zero net momentum Attitude knowledge: 0.02 3σ each axis LV Compatibility: ESPA, ESPA Grande, Minotaur,Pegasus XLBCP SEPSatConcept34
General AtomicsElectromagnetic SystemsHeritage / Schedule Information: ESPA Grande 300kg class LEO spacecraft 6 to be launched on falcon heavy for COSMIC2/FORMOSAT-7 constellation Same dual redundant architecture used in allLEO satellitesOrbital Test Bed - XCompany Information:Product Information: Dave Robie, David.Robie@ga.com, 858-8606708 Capabilities include engineering and satellitesubsystems. payload mass capacity 100kg payload power 300w OAP 3 axis control, ideal for remote sensingapplications 7 year life 1 Gbps downlink capacity launch 2021/22 Falcon SSO different LTDNsavailable, 500-600km6/13/201935
Millennium Space SystemsVertically Integrated, End-to-end Spacecraft Heritage / Schedule Information: Flight heritage AQUILA-M1 spacecraft launchedMission Prime System Integratoron 06 Feb 2011 hosting multiple payloads Flight heritage ALTAIR Pathfinder spacecraftcommercially deployed off of ISS on 17 May 2017hosting numerous technology components Flight heritage ALTAIR-E1 spacecraft launched on 04 May 2019 toISS and to be deployed in Jun 2019 Space-qualified AQUILA-M8 spacecraftmanifested on 2020 launch, dedicated payload Several more ALTAIR follow-on spacecraftwith planned launches in 2019 through 2020 Several RWA-1000s and processors on-orbitOrganization Information: Jason Kim, Vice President of Strategic Planning (310) 683-5884 Jason.kim@millennium-space.com Website: www.millennium-space.com Location: El Segundo, CA (150,000 sq-ft factory) No. Employees: 350 and growing Founded: in Nov 2001 ( 18 years in business) Acquired by The Boeing Company in Sep 2018, operatingas a non fully-integrated wholly owned subsidiary Customers: DoD, IC, NASA, Commercial GSA Schedule: RWA-1000 and more to come6/13/2019Product / Service Information:RAPTOR ProductsSpacecraft bus Longer life Higherperformance Selective to fullredundancy Moderate to highpower Small to mediumlaunch rideshareSpacecraft bus Shorter life High performance,tech refresh ESPA class Single string,selectiveredundancy Small to moderatepowerSpacecraft bus Miniaturizedcutting edgetechnology in 6Uto 12U compactform factor 100s of spacevehicles launchedoff dedicated orrideshareSubsystems RWAs & CMGs Star trackers Batteries IMUs Software DefinedRadios Antennas Processors SADAs And more†In addition to spacecraft bus and subsystems products, we provide SEIT, rapidprototyping, launch integration, launch support, and mission operations services36
Moog - OMVHeritage / Schedule Information: OMV based on flight heritage ESPA Ring(example EAGLE and LCROSS mission) All other elements (avionics, propulsion, power,comm, GNC) are TRL 9 and many sourced fromwithin Moog reducing cost and schedule Modular and scalable architecture to meetmission needs from short life commercial LEO tugto 5 year Class C operational mission beyondEarth Orbit CDR level, flight readiness at ATP 24 monthsCompany Information:Product Information: Christopher Loghry, cloghry@moog.com 720-289-7041 or 818-734-3445 www.moog.com/space Moog is a 2.5B company with 11,000 employeesin locations in 25 countries Moog is headquartered in East Aurora, NY andhas Space locations all over the US Moog was founded in 1951 and has supportednearly every single major space program includingApollo, Space Shuttle, EELV, and ISS Orbital Maneuvering Vehicle (OMV) leveragesRideshare for low-cost access to space OMV provides standalone power, propulsion,avionics, and communication as Free Flyer OMV can be used to achieve optimal orbits ofspacecraft or other payloads including BeyondEarth Orbit OMV can also act as a hosted payload platformfor payloads and be part of a system architecture(e.g. Comm Relay in Hub & Spoke system)6/13/201937
Northrop GrummanInnovation SystemsHeritage / Schedule Information: ESPAStar is Northrop Grumman’s Innovative ESPA-BasedPropulsive Satellite Platform–Design Based on Fight Proven AFRL’s EAGLEProgram Six ESPA Payload Slots Provide for Combinations of Hostedand/or Separable Payloads GEO Orbit Baseline–Organization Information:Carol WelschSenior Director of Business DevelopmentCarol.welsch@ngc.com(571) 342 0100-OrTim Rumford, P.E.ESPAStar Program DirectorTimothy.rumford@ngc.com(571) 447 61736/13/2019GTO, MEO, and LEO Variants Provides Standardized Interfaces, C3, Onboard Processing Compatible with All ESPA-Capable Launch VehiclesProduct / Service Information: Commercial-like production line reduces cost, schedule, and risk––Rolling inventory enables 22 month ATP to ILC scheduleParts commonality across multiple spacecraft product lines Modular ESPA-based Design Provides Mission Flexibility–––Open and published standard payload interfacesEnhancements available to meet unique user needsMature ICD and User’s Guide Designed to Maximize Opportunities for Launch–––Supports Variety of Payload Sizes (ESPA/Nano/CubeSat)Supports Combinations up to 12 Separating Payloads or 6 HostedPayloadsStackable Configurations MMSOC 2.1/EGS Compliant–Northrop Grumman’s Maestro TT&C38
TacSat‐2OG2STPSat‐5DSXHeritage / Schedule Information: TacSat-2, Launched December 2006, 0.5mGEOINT mission, low jitter, high-performance Orbcomm Generation 2 (OG2), Launched 2014& 2015, stacked ESPA, 17 satellites, productionline rate 1 satellite / month, ultra quiet EMI/EMC STPSat-5, Launched December 2018, greenpropellant, 5 payloads, common payload interface Deployable Structures Experiment (DSX), freeflying ESPA ring spacecraft, investigate persistentsmallsats for C3ISR in MEO, Launched Summer 19Company Information:Product Information: Tim Flora (720) 407-3247 Ext: 173247 Tim.Flora@sncorp.com https://www.sncorp.com/ Louisville, Colorado, USA 800 Space Systems Group employees Established in 1963 Prime Integrator and Spacecraft Bus provider Active SmallSat Projects Include: OrbcommGeneration 2, STPSat-5, DSX, SN-50, Other Orbit: LEO, MEO, GEO, or deep space Inclination: As required by mission Stabilization: 3-axis, zero net momentum Attitude Knowledge: 0.01 or 0.001 LV Compatibility: ½ ESPA, ESPA, ESPA Grande,Minotaur 1/4, Falcon 9 Bus & P/L Example:6/13/2019––SN-50 ESPASTPSat-5 (LEO)39
NASA & USAF HP's on a Commercial Bus NASA's GeoCarb HP on a Commercial Bus 6/13/2019. Rideshare / ESPA Heritage: Capacity v. Flown the lost opportunity of empty slots 6/13/2019 19 Mission L/V Carrier Launch Date S/C Capacity S/C Flown Empty Slots STP-1 Atlas 5 ESPA March 2007 6 4 2 .
Transport Payload Testing How to Verify the (Rx) Payload Data of a Frame MD1230B/MP1590B Data Quality Analyzer/Network Performance Tester Introduction This application note explains the steps necessary to verify the (Rx) payload data within an Ethernet frame. . Each stream can be c
energy: 60.0 ft-lbf 34 Section Mass Descent Velocity (Payload attached) Descent Velocity Kinetic Energy (Payload attached) Kinetic Energy Nosecone 0.2907 slugs 14.5 ft/s 12.8 ft/s 30.6 ft-lbf 23.9 ft-lbf Nosecone w/ Payload 0.5704 slugs 14.5 ft/s N/A 60.0 ft-lbf N/A Payload 0.2797 slugs 14.5 ft/s N/A 29.4 ft-lbf N/A Midsection 0.3457 slugs
expansions were necessary for it in the 19th century. It seeks to what meant by manifest Destiny, what are the origins of it in America, and what the main factors behind that expansion from the west forward. 1.2 Manifest Destiny Defined Manifest Destiny is an ideological concept, which is a historical progress in the United
Apr 01, 2008 · Ship Notice/Manifest - 856 856 Ship Notice/Manifest Functional Group SH This Draft Standard for Trial Use contains the format and establishes the data contents of the Ship Notice/Manifest Transaction Set (856) for use within the context of an Electronic Data Int
Warm Up: Review Manifest Destiny In your notebooks answer the following questions about the painting: 1. What is the concept of Manifest Destiny? 2. Choose 3 Objects in the picture and describe those objects and how those relate to the concept of Manifest Destiny. Manifest Destiny was the concept that it was
New manifest procedures begin for any manifest initiated by the generator starting June 30, 2018. Existing paper manifest form is being replaced with a new 5-copy form. The new form will be effective starting on June 30, 2018. Generators may continue to use paper manifests after June 30, 2018.
The Orange County Transportation Authority (OCTA) is seeking to partner with . interest in the environment is a great way to leverage the OCTA Rideshare Program. With 91 percent of Americans now owning a cell phone, 63 percent of them using their . bus service network and to provide trips outside regu
ASME A17.1-2013 / CSA B44-13 2.25.4.1.1 Emergency Terminal Speed-Limiting Device New requirement to apply the emergency brake if the main brake fails to slow the car down when ETSL actuated. Both brakes may be applied but max deceleration is 9.81 m/s2. Reduced stroke buffer ETSL Broken Shaft - Main brake does not work Emergency brake applied when car fails to slow down as intended Car below .
