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Engine Model: HM-16. Designer: Mitsubishi. Gross Mass: 100 kg (220 lb). Propellants: Solid. Diameter: 0.17 m (0.54 ft). Length: 1.00 m (3.20 ft). Country: Japan.
Engine Model: K160. Designer: ISAS. Gross Mass: 100 kg (220 lb). Empty Mass: 20 kg (44 lb). Propellants: Solid. Burn time: 5.30 sec. Diameter: 0.16 m (0.52 ft). Length: 2.40 m (7.80 ft). Country: Japan.
Engine Model: NAL-16. Designer: Mitsubishi. Gross Mass: 100 kg (220 lb). Empty Mass: 40 kg (88 lb). Propellants: Solid. Thrust(vac): 10.000 kN (2,248 lbf). Burn time: 14 sec. Diameter: 0.17 m (0.54 ft). Length: 3.90 m (12.70 ft). Country: Japan.
Engine Model: S-160. Designer: ISAS. Gross Mass: 100 kg (220 lb). Propellants: Solid. Diameter: 0.16 m (0.52 ft). Length: 3.90 m (12.70 ft). Country: Japan.
Engine Model: S-A. Designer: Mitsubishi. Gross Mass: 100 kg (220 lb). Propellants: Solid. Diameter: 0.16 m (0.52 ft). Length: 2.80 m (9.10 ft). Country: Japan.
Engine Model: S-B. Designer: Mitsubishi. Gross Mass: 100 kg (220 lb). Propellants: Solid. Diameter: 0.16 m (0.52 ft). Length: 2.80 m (9.10 ft). Country: Japan.
Engine Model: S-C. Designer: Mitsubishi. Gross Mass: 100 kg (220 lb). Propellants: Solid. Diameter: 0.16 m (0.52 ft). Length: 2.80 m (9.10 ft). Country: Japan.
K160 used on Rocket Stages - Used on stage: HM-16. on launch vehicle: S.
- Used on stage: NAL. on launch vehicle: S.
- Used on stage: S-160. on launch vehicle: S.
- Used on stage: S-A. on launch vehicle: S.
- Used on stage: S-B. on launch vehicle: S.
- Used on stage: S-C. on launch vehicle: S.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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