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
MR-125
LLNL solid rocket engine. Astrid first stage.

AKA: Astrid-1. Status: Retired 1994. Thrust: 400 N (80 lbf). Gross mass: 20 kg (44 lb). Unfuelled mass: 8.00 kg (17.60 lb). Burn time: 30 s. Height: 1.90 m (6.20 ft). Diameter: 0.17 m (0.55 ft).



Country: USA. Launch Vehicles: Astrid test vehicle. Propellants: Solid. Stages: MR-125. Agency: Livermore.

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