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Page 1 NASA report to the CCSDS Management Council November 2009 ESA ESTEC, Noordwijk, Netherlands Mike Kearney NASA 256-544-2843 Mike.Kearney@nasa.gov
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Page 2 Agenda NASA CCSDS support Note – No NASA org update (no change) Overall NASA program schedule (AMPM) Recent missions Upcoming missions Advanced Comm Technology Efforts
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Page 3 NASA CCSDS Participation NASA Rapporteurs (lead representatives) 1.2 Security WGHowie WeissSparta 1.3 Information Architecture WGDan CrichtonJPL 1.4 SANA WGKelvin NicholsMSFC 1.5 Delta-DOR WGJim BorderJPL 1.6 Time Code Format WGEd GreenbergJPL XML SIG Lou ReichGSFC/CSC Registry/Repository SIGDan CrichtonJPL 2.1 Data Archive Ingestion WGJohn GarrettGSFC 2.2 Navigation WGDave BerryJPL 2.3 Info. Pack. & Registries WGLou ReichGSFC/CSC 2.4 S/C Mon + Control WGLindolfo MartinezJSC 2.5 Digital Repository Audit/Cert (RAC) WGJohn GarrettGSFC/CSC 3.3 Service Mgmt. WGErik BarkleyJPL 3.6 Cross Support Transfer Services WGTim RayGSFC 3.7 Cross Support Architecture WGFred BrosiJPL/GST 4.1 Onboard Subnetwork Services WGGlenn RakowGSFC 4.3 Onboard Application Services WGScott BurleighJPL 4.4 Onboard Wireless WGKevin GiffordCU 5.1 RF & Modulation WGDennis LeeJPL 5.2 Space Link Code/Sync. WGVictor SankGSFC 5.3 Multi/Hyper Data Compression WGAaron KielyJPL 5.4 Space Link Protocols WGGreg KazzJPL 5.6 Ranging Working GroupSteve LevitskiGSFC 5.8 High Rate Uplink WGGreg KazzJPL Long Erasure Codes BOFFabrizio PollaraJPL Space Data Link Layer Security BOFHowie WeissSparta 6.5 Asynch. Messaging Service WGScott BurleighJPL 6.6 IP-over-CCSDS Links WGGreg KazzJPL 6.8 Delay Tolerant Networking WGKeith ScottJPL/Mitre 6.9 Motion Imagery and Applications WGRodney GrubbsMSFC 6.10 Voice WGMichael PetersenJSC/LMIT NO CHANGE
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Page 5 Recent Missions
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Page 6 Recent Missions - Ares 1-X Sucessful launch on Oct 28, 2009 2 minute powered flight, 6 min. total Splashdown 150 mi. downrange Parachute deployment problem Booster damaged on impact Successful shakedown flight, testing Ares design concepts
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Page 7 Recent Missions - LCROSS LCROSS impact on moon on 9 October Centaur stage impacted first while “shepherd” vehicle recorded data Nine LCROSS instruments successfully captured each phase of the impact sequence: the impact flash, the ejecta plume, and the creation of the Centaur crater Centaur impact left crater 92 ft. (28 m) wide Plume of vapor and fine debris detected Spectrographic and other analysis is underway.
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Page 8 Recent Missions - Messenger Launch: August 3, 2004 aboard a Boeing Delta II rocket Gravity assist flybys Earth, August 2005; Venus, October 2006, June 2007; Mercury, January 2008, October 2008, September 2009 Enter Mercury orbit: March 2011. Mission Plan : Orbit for one Earth year, studying Composition and structure of Mercury’s crust Topography and geologic history The nature of its thin atmosphere and active magnetosphere, The makeup of its core and polar materials
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Page 9 Recent Missions - Spirit Mars Rover Spirit has been operating on Mars for 69 mos. Became stuck in soft soil in Spring 2009. Light soil in image below was exposed after Spirit attempted to free it’s wheels. Also battling memory problems
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Page 10 Recent Missions - Opportunity Ran across three meteorites laying on the ground within a few weeks of each other (700 meters apart) Heading towards Endeavour Crater
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Page 11 Upcoming Missions
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Page 12 Remaining Shuttle Flights FlightDateYearShuttleCrew sizeDurationNotes STS-129November 162009Atlantis6/7~11d ISS assembly flight ULF3: ExPRESS Logistics Carriers (ELCs) 1 & 2. STS-130February 42010Endeavour6~11d ISS assembly flight 20A: Node 3 and Cupola. STS-131March 182010Discovery7~11d ISS assembly flight Utility and Logistics Flight 4: Multi-Purpose Logistics Module Leonardo. STS-132May 142010Atlantis6~11d ISS assembly flight 19A: Mini-Research Module 1. Final planned flight of Atlantis. STS-134July 292010Endeavour6~12d ISS assembly flight ULF6, ELC 4, ROEU, Alpha Magnetic Spectrometer. Final planned flight of Endeavour. STS-133September 162010Discovery6~10d ISS assembly flight ULF5, MPLM Leonardo, (to be left pemanently attached), ELC 3. Final flight of Discovery; final Shuttle flight of the program.
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Page 13 Constellation Activities An Orion crew module Ground Test Article at the NASA Michoud Assembly Facility in New Orleans. Photo Credit: NASA A demonstration test of the main parachute test equipment for the Orion crew exploration vehicle completed Oct. 2, 2009 Ground vibration test of the Orion Launch Abort System, August 2009 Orion flight test crew module - used for the Orion Pad Abort flight test starting early 2010 NASA conducted complete launch simulations of an Orion mission to ISS to verify operations tools and processes for Constellation Mission Ops. IMSim (Integrated Mission Simulation), gave a networked system of high fidelity “physics” simulations, performed the real time launch and ascent simulation and post insertion burn. The DON (Distributed Observer Network) distributed the IMSim visualizations to remote team members and saved them for playback later. Both tools are part of the Constellation Modeling and Simulation Team (MaST).
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Page 14 TDRSS Fleet Update Tracking and Data Relay Satellite (TDRSS K/L) Procurement for two replenishment s/c functionally equivalent to TDRSS series 2 (H,I,J) Launch date: TDRSS K April 2012TDRSS L April 2013 TDRSS Fleet Status Preparations underway to retire F-1 after 26 years of service
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Page 15 Advanced Comm Technology efforts
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Page 16 LADEE Optical Comm Demonstration ~ 2012 10/31/2008 16 LADEE Terrestrial Photon-Counting Array Rx Orbital terminal Inertial-stabilization Fully-gimbaled Low size, weight, & power design Lunar Atmosphere and Dust Environment Explorer (LADEE) Will characterize the lunar atmosphere and lunar dust environment. Will demonstrate optical comm technology Orbiter-to-Earth Laser Communications 622 Mbps downlink (O-E) 16 Mbps uplink (E-O) Sub-cm ranging
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Page 17 Software Defined Radio Testbed on ISS 17 SCAN Testbed is located on the ISS port (P3) ELC, mounted on the starboard side of the P3 ELC on the zenith/ram corner. HTV Launch to ISS in 2011 SCaN on-orbit Testbed consist of: Three Software Defined Radios Ka-Band Capability S-band Capability GPS Experiment Testbed
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