Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Ares Stage 2
LOx/LH2 propellant rocket stage. Second stage proposed later in design stage by NASA for launch of CEV into low earth orbit. All masses estimated.

Status: In development. Thrust: 1,113.00 kN (250,212 lbf). Gross mass: 172,000 kg (379,000 lb). Unfuelled mass: 13,200 kg (29,100 lb). Specific impulse: 465 s. Burn time: 640 s. Height: 16.00 m (52.00 ft). Diameter: 10.00 m (32.00 ft). Span: 10.00 m (32.00 ft).



Country: USA. Launch Vehicles: Ares I-X, Ares V. Propellants: Lox/LH2.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use