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1 Ares I Crew Launch Vehicle ♦ ~25-mT payload capacity ♦ 2-Mlb gross liftoff weight ♦ 309 ft in length Upper Stage • 280-klb Liquid Oxygen/Liquid Hydrogen (LOX/LH 2) Stage • 5.5-m Diameter • Aluminum-Lithium (Al-Li) Structures • Instrument Unit and Interstage • RCS / Roll Control for First Stage flight • CLV Avionics System First Stage • Derived from Current Shuttle Reusable Solid Rocket Motor/Booster (RSRM/B) • Five Segments/Polybutadiene Acrylonitride (PBAN) Propellant • Recoverable • New Forward Adapter Upper Stage Engine • Saturn J-2 Derived Engine (J-2X) • Expendable

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Page 1: Ares I Crew Launch Vehicle - NASA

1

Ares I Crew Launch Vehicle

♦~25-mT payload capacity♦2-Mlb gross liftoff weight♦309 ft in length

Upper Stage• 280-klb Liquid Oxygen/Liquid Hydrogen

(LOX/LH2) Stage• 5.5-m Diameter• Aluminum-Lithium (Al-Li) Structures• Instrument Unit and Interstage• RCS / Roll Control for First Stage flight• CLV Avionics System

First Stage• Derived from Current Shuttle Reusable

Solid Rocket Motor/Booster (RSRM/B)• Five Segments/Polybutadiene

Acrylonitride (PBAN) Propellant• Recoverable• New Forward Adapter

Upper Stage Engine• Saturn J-2 Derived Engine (J-2X)• Expendable

Page 2: Ares I Crew Launch Vehicle - NASA

2

Ares V Cargo Launch Vehicle

Composite Shroud

Earth Departure Stage• LOx/LH2• One J2X+ Engine• Al-Li Tanks/Structures

Core Stage• LOx/LH2• Five RS68 Engines• Al-Li Tanks/Structures

Five Segment RSRBs

Ascent StageDescent Stage LSAM

Interstage

Upper Stage Engine• Saturn J-2 Derived Engine (J-2X)• Expendable

♦~130-mT payload capacity♦7.4-Mlb gross liftoff weight♦358 ft in length


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