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
Atlas MA-2
Part of Atlas MA engine series Family
LOx/Kerosene propellant rocket stage. .

Status: Out of production. Thrust: 1,517.42 kN (341,130 lbf). Gross mass: 3,050 kg (6,720 lb). Unfuelled mass: 3,050 kg (6,720 lb). Specific impulse: 282 s. Specific impulse sea level: 248 s. Burn time: 135 s. Diameter: 4.90 m (16.00 ft). Span: 4.90 m (16.00 ft).

No Engines: 2.



Country: USA. Engines: XLR89-5. Launch Vehicles: Atlas Able, Atlas B, Atlas C, Atlas D, Atlas C Able, Atlas D Able, Atlas Agena A, Atlas LV-3B / Mercury, Atlas Centaur, Atlas Centaur D. Propellants: Lox/Kerosene.

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