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
M-3B-J
Part of M-3B-Mu Family
Nissan solid rocket engine. In development. Used on J-1 launch vehicle. First flight 1996.

AKA: M-3B. Status: In development. Number: 1 . Thrust: 132.10 kN (29,697 lbf). Gross mass: 3,600 kg (7,900 lb). Unfuelled mass: 300 kg (660 lb). Specific impulse: 294 s. Burn time: 87 s. Height: 2.70 m (8.80 ft). Diameter: 1.50 m (4.90 ft).

Area Ratio: 52.



Country: Japan. Launch Vehicles: J-1. Propellants: Solid. Stages: M-3B-Mu. Agency: Nissan.

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