Rideshare Payload User's Guide - Storage.googleapis
RIDESHAREPAYLOADGUIDESeptember 2021COPYRIGHTSubject to the existing rights of third parties, Space Exploration Technologies Corp. (SpaceX) is the owner of the copyrightin this work, and no portion hereof is to be copied, reproduced, or disseminated without the prior written consent ofSpaceX.No U.S. Export Controlled Technical Data or Technology.
RIDESHARE PAYLOAD USER’S GUIDETABLE OF CONTENTS123INTRODUCTION . 11.1Rideshare Payload User’s Guide Purpose . 11.2Company Description . 21.3Rideshare Program Overview . 21.4Falcon 9 Program. 31.5Pricing . 3PERFORMANCE . 42.1Mass Properties . 42.2Launch Windows . 42.3Separation Attitude and Accuracy . 52.4Separation Rates and Velocity. 52.5Payload Maneuvers and Deployments . 6ENVIRONMENTS . 73.1Transportation Environments . 73.2Cleanroom Environments . 73.3Flight Environments. 83.3.1Loads . 83.3.2Sine Vibration . 93.3.3Acoustic . 103.3.4Shock. 113.3.5Random Vibration . 123.3.6Electromagnetic . 133.3.7Fairing Internal Pressure . 143.3.8Payload Temperature Exposure During Flight . 153.3.9Free Molecular Heating . 153.3.10Payload Conductive Boundary Temperatures . 153.3.11Contamination . 163.44Environmental Verification Testing . 173.4.1Verification Approach . 173.4.2Documentation Requirements . 173.4.3Payload Unit Test Levels . 183.4.4Containerized CubeSat Unit Test Levels . 193.4.5Metallic Structure Unit Test Levels . 203.4.6Functional Testing Requirements . 20INTERFACES . 214.1Mechanical Interfaces . 214.1.1Launch Vehicle Coordinate Frame . 214.1.2Launch Vehicle Fairing. 21 Space Exploration Technologies Corp. All rights reserved. No U.S. Export Controlled Data.ii
RIDESHARE PAYLOAD USER’S GUIDE4.1.3Payload Coordinate Frame . 224.1.4Mechanical Interface Ring . 224.1.5Payload Available Volume . 234.1.6Mechanical Interface Compatibility . 264.256Electrical Interface . 264.2.1Standard Offering Interface . 264.2.2Deployment Channel Properties . 274.2.3Breakwire Channel Properties . 274.2.4Umbilical Channel Properties . 284.2.5Flight Harness Design . 294.2.6Connectivity during Payload Processing . 294.2.7Ground Harness Design . 294.2.8Timing Services . 304.2.9Electrical Interface Compatibility . 30LAUNCH SITE FACILITIES . 315.1Facility Access and Working Hours . 315.2Customer Offices . 315.3SpaceX Payload Processing Facility (PPF) . 315.4Launch Complex . 325.5Launch Countdown Monitoring . 32MISSION INTEGRATION AND SERVICES. 336.1Contracting . 336.2US Export and Import Control Laws . 336.3Mission Management. 336.4Program Documentation . 346.4.1Interface Control Document (ICD) . 346.4.2Launch Campaign Plan. 346.4.3Program Status, Meetings, Working Groups and Reviews . 346.5Customer Responsibilities. 356.5.1Transportation . 356.5.2Hardware, Processing and Integration . 356.5.3Hazardous Procedures . 366.5.4Entry and Exit Visas . 366.5.5Anomaly, Mishap, Accident or Other Event . 366.5.6Payload Licensing and Registration . 366.5.7Coordination with Space Situational Awareness Agencies . 366.6SpaceX Responsibilities . 376.6.1Launch Scheduling . 376.6.2Transportation Services . 376.6.3Payload Integration and Associated Hardware . 37 Space Exploration Technologies Corp. All rights reserved. No U.S. Export Controlled Data.iii
RIDESHARE PAYLOAD USER’S GUIDE76.6.4Photographic Services . 376.6.5Security . 386.6.6Launch Campaign . 386.6.7Facility Support and Operations . 386.6.8Licensing and Registration . 386.6.9Mission Integration Analyses . 39OPERATIONS . 417.1Overview and Schedule . 417.2Rideshare Payload Delivery and Transportation . 417.3Rideshare Payload Processing . 417.4Joint Operations and Integration . 417.5Launch Operations . 417.5.1Organization . 417.5.2Launch Control . 427.5.3Rollout and Pad Operations . 427.5.4Countdown . 427.5.5Recycle and Scrub . 427.68Flight Operations . 42SAFETY . 438.1Safety Requirements . 438.2Hazardous Systems and Operations . 438.3Waivers . 43APPENDIX A: MECHANICAL INTERFACE (RINGS AND VOLUMES) . 44APPENDIX B: PAYLOAD DYNAMIC MODEL REQUIREMENTS. 52APPENDIX C: PAYLOAD CAD MODEL REQUIREMENTS . 55APPENDIX D: PAYLOAD ENCAPSULATION & LAUNCH READINESS CERTIFICATES . 56APPENDIX E: DELIVERY FORMAT OF SEPARATION STATE VECTOR . 58APPENDIX F: PAYLOAD LICENSING CERTIFICATION. 59APPENDIX G: DELIVERABLES DESCRIPTION .60APPENDIX H: PAYLOAD CONSTITUENTS . 64APPENDIX I: OPTIONAL SERVICES . 65APPENDIX J: DEFINITIONS . 66 Space Exploration Technologies Corp. All rights reserved. No U.S. Export Controlled Data.iv
RIDESHARE PAYLOAD USER’S GUIDEACRONYMSAFSPCMAN . Air Force Space Command ManualATM . acceleration transformation matrixBPSK . binary phase shift keyingCAD .computer-aided designCCSFS . Cape Canaveral Space Force StationCG. center of gravityCLA. coupled loads analysisCSLA . Commercial Space Launch ActCSpOC .Combined Space Operations CenterDSSS . direct-sequence spread spectrumDRM . data recovery matrixDTM . displacement transformation matrixEAR . export administration regulationsECEF . earth-centered, earth-fixedEGSE . electrical ground support equipmentEIRP . equivalent isotropically radiated powerEMI . electromagnetic interferenceEMISM . EMI safety marginFAA . Federal Aviation AdministrationFCC .Federal Communications CommissionFEM. finite element modelFM . frequency modulationFMCW.frequency modulation continuous waveFOD . foreign object debrisGOP . ground operations planGPS . global positioning systemGSE . ground support equipmentHVAC . heating, ventilation and air conditioningICD . interface control documentIGES . initial graphics exchange specificationIRIG . inter-range instrumentation groupITAR .
Section 2 Mass versus C.G. definition updated Clarifications on deployment direction Updated CubeSat and multi-deploy velocities Updated Launch Vehicle pre-separation rates Section 3 Updated cleanroom environments Updated combined loads including clarification on random vibration interaction
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
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
TLE Two Line Element . P a g e 8 Intellectual FF-0005001 - Alpha 1.0 Payload Users Guide Rev 01 Property Designation. . Alpha is a two-stage launch vehicle capable of delivering 400 kg of payload to LEO. The first variant, Alpha 1.0, utilizes efficient technologies such as composite
JWT, a payload. a hash, and an encryption algorithm used for the hash. The payload contains the user ID, the timestamp indicating when the JWT was issued, and a JWT expiry timestamp. The header and payload is base64 encoded and hashed with HMAC using SHA-256 and a secret. When the authentication mid
Penguin B can handle up to 11.5 kg of combined fuel and payload weight. Modular composite structure, fast assembly, large access hatches, removable payload bay, are the key features of the Penguin B innovative design. Available as an airframe ready for the autopilot and payload integration. PENGUIN B UAV PLATFORM Datasheet v 2.0 Penguin B platform
Alfredo López Austin and Leonardo López Luján 18.3. Schematic map of the successive relocations of the Tizoc Stone (1–5) and the Archbishop’s Stone (A–B), by Tenoch Medina. was the one that has been unearthed for the second time at the site where the Cathedral of Mexico City is being constructed. This stone now stands at the western doorway of the church. The ancients call this the .
