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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.
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