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-V-4
Part of M-3 Family
Nissan solid rocket engine. Used on M-V launch vehicle. First flight 1997.

Status: Active. Number: 7 . Thrust: 52.00 kN (11,690 lbf). Gross mass: 1,430 kg (3,150 lb). Unfuelled mass: 118 kg (260 lb). Specific impulse: 298 s. Burn time: 73 s. Height: 1.50 m (4.90 ft). Diameter: 1.20 m (3.90 ft).

Chamber Pressure: 49.00 bar. Area Ratio: 89.



Country: Japan. Launch Vehicles: M-V, M-V KM. Propellants: Solid. Stages: M-V-4. 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