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Ares V RFI Point of Departure Information Package

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Presentation on theme: "Ares V RFI Point of Departure Information Package"— Presentation transcript:

1 Ares V RFI Point of Departure Information Package
National Aeronautics and Space Administration National Aeronautics and Space Administration National Aeronautics and Space Administration Ares V RFI Point of Departure Information Package

2 Ares V Point of Departure Configuration
Altair Lunar Lander Interstage Solid Rocket Boosters (2) Two recoverable 5.5-segment PBAN-fueled, steel-casing boosters (derived from current Ares I first stage J–2X Payload Shroud RS–68B Engines (6) Loiter Skirt Earth Departure Stage (EDS) One Saturn-derived J–2X LOX/LH2 engine (expendable) 10 m (33 ft) diameter stage Aluminum-Lithium (Al-Li) tanks Composite structures, Instrument Unit and Interstage Primary Ares V avionics system Core Stage Six Delta IV-derived RS–68B LOX/LH2 engines (expendable) Composite structures Gross Lift Off Mass: 3,704.5 mT (8,167.1k lbm) Integrated Stack Length: 116 m (381 ft) Payload Adapter National Aeronautics and Space Administration

3 Point of Departure Earth Departure Stage
Altair (Lander) Adapter LH2 Tank Intertank Aft Skirt EDS J-2X Engine Forward Skirt/ Instrument Unit Avionics Interstage LOX Tank Aluminum-Lithium (Al-Li) propellant tanks Composite dry structure 10 m (33 ft) outer diameter Derived from Ares I Upper Stage 4-day on-orbit loiter capability prior to Trans-Lunar Injection (TLI) Maintains Orion/Altair/EDS stack attitude in Low Earth Orbit prior to TLI Burn EDS provide 1.5 kW of power to Altair from launch to TLI Loiter Skirt National Aeronautics and Space Administration

4 Point of Departure Core Stage
Forward Skirt & Core Stage Avionics LH2 Tank & Systems Tunnel LOX Tank Intertank & Thrust Beam Aft Skirt Core Stage RS-68B Engines Aluminum-Lithium (Al-Li) propellant tanks Composite dry structure 10 m (33 ft) outer diameter Derived from Shuttle External Tank Engine Thrust Structure Engine Compartment National Aeronautics and Space Administration

5 Example Ongoing Ares V Trades
Composite case/HTPB solid rocket booster Biconic vs. ojive shaped payload shroud Core stage engine layout National Aeronautics and Space Administration

6 Ares V Point of Departure Development Schedule
National Aeronautics and Space Administration 7527.6 6

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