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H-1-3
Part of UM-129 stage series
Nissan solid rocket engine. Used on H-1 launch vehicle. First flight 1986.

AKA: UM-129A. Status: Retired 1992. Number: 9 . Thrust: 77.00 kN (17,310 lbf). 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).

Country: Japan. Launch Vehicles: H-1, H-1 6R. Propellants: Solid. Stages: H-1-3. Agency: Nissan.
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