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Engine Model: L735. Designer: ISAS. Gross Mass: 5,000 kg (11,000 lb). Empty Mass: 2,945 kg (6,492 lb). Propellants: Solid. Thrust(vac): 410.000 kN (92,170 lbf). Burn time: 29 sec. Diameter: 0.74 m (2.42 ft). Length: 8.40 m (27.50 ft). Country: Japan.
Engine Model: L735(1/3). Designer: ISAS. Gross Mass: 2,500 kg (5,500 lb). Propellants: Solid. Thrust(vac): 118.000 kN (26,527 lbf). Burn time: 38 sec. Diameter: 0.74 m (2.42 ft). Length: 3.90 m (12.70 ft). Country: Japan.
Engine Model: NAL-735. Designer: NASDA. Gross Mass: 4,700 kg (10,300 lb). Propellants: Solid. Thrust(vac): 250.000 kN (56,200 lbf). Burn time: 49 sec. Diameter: 0.74 m (2.42 ft). Length: 9.00 m (29.50 ft). Country: Japan.
Engine Model: SB-735. Designer: Nissan. Gross Mass: 5,100 kg (11,200 lb). Empty Mass: 1,080 kg (2,380 lb). Propellants: Solid. Thrust(vac): 327.800 kN (73,692 lbf). Thrust(sl): 296.700 kN (66,701 lbf). Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 38 sec. Diameter: 0.73 m (2.39 ft). Length: 8.25 m (27.06 ft). Chambers: 1. Country: Japan. First Flight: 1969. Last Flight: 1995. Flown: 48.
Engine Model: ST-735-1. Designer: ISAS. Gross Mass: 7,400 kg (16,300 lb). Propellants: Solid. Diameter: 0.74 m (2.42 ft). Length: 4.60 m (15.00 ft). Country: Japan.
Engine Model: ST-735-2. Designer: ISAS. Gross Mass: 4,000 kg (8,800 lb). Propellants: Solid. Diameter: 0.74 m (2.42 ft). Length: 2.00 m (6.50 ft). Country: Japan.
ST-735 used on Rocket Stages
- Used on stage: SB-735. on launch vehicle: Mu.
- Used on stage: SB-735. on launch vehicle: S.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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