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-10
Nissan solid rocket engine. Mu-4S first stage.

AKA: Mu-4S-1. Status: Retired 1979. Thrust: 737.00 kN (165,684 lbf). Gross mass: 26,600 kg (58,600 lb). Unfuelled mass: 5,907 kg (13,022 lb). Burn time: 61 s. Height: 13.00 m (42.00 ft). Diameter: 1.41 m (4.62 ft).



Subtopics

M-20 Nissan solid rocket engine.

M-22 Nissan solid rocket engine.

M-13 Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969.

M-23-Mu Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969. Mu-3S second stage.

M-23-J Nissan solid rocket engine. In development. Used on J-1 launch vehicle. First flight 1996. Solid propellant rocket stage. Version for J-1 F2 has 300 kg heavier empty mass. J-1 second stage.

Country: Japan. Launch Vehicles: Mu-1, Mu-3D, Mu-4S, Mu-3C, ETV. Propellants: Solid. Stages: M-10. 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