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UM-129A


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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 UM-129A Part of UM-129 stage series Nissan solid rocket engine. In Production. Used in H-1-3.

Status: In Production. Thrust: 77.50 kN (17,423 lbf). Gross mass: 2,200 kg (4,800 lb). Unfuelled mass: 360 kg (790 lb). Specific impulse: 291 s. Specific impulse sea level: 220 s. Burn time: 68 s. Height: 2.34 m (7.67 ft). Diameter: 1.34 m (4.39 ft).

Thrust (sl): 58.600 kN (13,174 lbf). Thrust (sl): 5,973 kgf. Area Ratio: 54.

Country: Japan. Propellants: Solid. Agency: Nissan. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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