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LDCM Spacecraft Status. Stylist. Bill Anselm, LDCM Observatory June 23, 2009. Manager. INTRODUCTION. Spacecraft Context Implementation Status Schedule Spacecraft from a kit Launch support Summary. S-band SSA 1 kbps Forward 2 or 32 kbps Return. LDCM Observatory (OLI, TIRS). TDRSS.
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LDCM Spacecraft Status Stylist Bill Anselm, LDCM Observatory June 23, 2009 Manager
INTRODUCTION • Spacecraft Context • Implementation Status • Schedule • Spacecraft from a kit • Launch support • Summary
S-band SSA 1 kbps Forward 2 or 32 kbps Return LDCM Observatory (OLI, TIRS) TDRSS Link Color Code Green = S-band to / from LGN or NGN Yellow = Real-time X-band to LGN or ICs Orange = Playback X-band to LGN Pink = S-band to / from TDRSS LDCM Orbit 705 km circular sun sync, 10am DNLT 16-day repeat X-band Stored Science RT+PB or 2 PB @ 384 Mbps Potential IC Sites: ASN Alice Springs, Australia BJC Beijing, PRC BKT Bangkok, Thailand COA Cordoba, Argentina CUB Cuiaba, Brazil DKI Parepare, Indonesia GNC Gatineau, Canada HAJ Hatoyama, Japan HIJ Hiroshima, Japan HOA Hobart, Australia JSA Johannesburg, South Africa KIS Kiruna, Sweden MPS Maspolomas, Spain MTI Matera, Italy PAC Prince Albert, Canada PF1 Poker Flat, Alaska SEK Seoul, Korea SGS Svalbard, Norway TFT Taipei Fixed Taiwan UPR University of Puerto Rico X-band RT Broadcast 384 Mbps S-band CMD uplink 1 or 32 kbps S-band RT downlink 32 kbps S-band combined Stored &RT TLM downlink 1 Mbps Alaska Ground Station Gilmore, AK Representative IC Canada Landsat Ground Station Sioux Falls, SD NASA GN Wallops Island, VA Atlas V VAFB Data rates shown are information rates, not modulation rates LDCM CONTEXT
IMPLEMENTATION STATUS • Spacecraft design is sound • Effective management in place • Highly talented and motivated team • Well on the road for October CDR
IMPLEMENTATION • Rapid Spacecraft Development Office • Unique “catalog-based” IDIQ contract • 8 Vendors; 18 Spacecraft • Selection is “rapid”; award-to-launch ~ non-RSDO • Fixed-price performance-based Delivery Order milestones • D. O. Management • Admin: CDRLs, studies, milestones • Technical: analyses, margins, requirements compliance • Deliverables: • Spacecraft/Observatory • Simulators (Interface, Observatory, Software Development) • Launch Support • Mission Operations Support
SPACECRAFT ROOTS GENERAL DYNAMICS ADVANCED INFORMATION SYSTEMS
SPACECRAFT KITTING Primary Structure Test Configuration Instrument Deck Primary Structure Propulsion Module
SPACECRAFT KITTING Instrument Deck Primary Structure SSR IEM Propulsion Module
SPACECRAFT KITTING Instrument Deck LCU Primary Structure Converter Box 2X CCU SSR OCXO 2X Battery IEM Propulsion Module
SPACECRAFT KITTING TAM 2X Instrument Deck LCU Primary Structure Converter Box 2X CCU ETR 3X SSR OCXO 2X Battery IEM CSS 12X Propulsion Module
Completed HPM SPACECRAFT KITTING TAM 2X Instrument Deck LCU Primary Structure Converter Box 2X CCU ETR 3X SSR OCXO 2X Battery IEM CSS 12X Propulsion Module
SPACECRAFT KITTING TAM 2X S-band Antenna 4X Instrument Deck Star Tracker 2X S-band Transceiver 2X IMU LCU Primary Structure Converter Box 2X X-band XMTR 2X CCU ETR 3X SSR RWA 6X TWTA 2X OCXO 2X Battery ECA 2X IEM CSS 12X Decryptor Propulsion Module
SPACECRAFT KITTING TAM 2X S-band Antenna 4X Instrument Deck Star Tracker 2X S-band Transceiver 2X IMU LCU PIE HIB 2X Primary Structure Converter Box 2X X-band XMTR 2X CCU ETR 3X SSR ECU RWA 6X GPS Antenna 4x TWTA 2X OCXO 2X Battery ECA 2X IEM CSS 12X GPS Receiver 2X Decryptor Propulsion Module
SPACECRAFT KITTING OLI TIRS TIRS Electronics 2X TAM 2X S-band Antenna 4X Instrument Deck Star Tracker 2X S-band Transceiver 2X IMU LCU PIE HIB 2X Primary Structure Converter Box 2X X-band XMTR 2X CCU ETR 3X SSR ECU RWA 6X GPS Antenna 4x TWTA 2X SADA OCXO 2X Battery ECA 2X IEM CSS 12X GPS Receiver 2X Decryptor Propulsion Module
SPACECRAFT KITTING OLI TIRS TIRS Electronics 2X TAM 2X S-band Antenna 4X Instrument Deck Star Tracker 2X S-band Transceiver 2X IMU LCU PIE Solar Array HIB 2X Primary Structure Converter Box 2X X-band XMTR 2X CCU ETR 3X SSR ECU RWA 6X GPS Antenna 4x TWTA 2X SADA OCXO 2X Battery ECA 2X IEM CSS 12X GPS Receiver 2X Decryptor Propulsion Module
LDCM USGS
SUMMARY • Design is sound • Good margins, buildable, testable, lots of heritage • Interfaces well covered • Simulators buy-down risk • Management and execution sound • Documents, risks, schedule • Planning sound • Progress monitored, good reserves • Great team in place • On to CDR!