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Engine Model: S-210. Designer: ISAS. Gross Mass: 200 kg (440 lb). Propellants: Solid. Diameter: 0.21 m (0.68 ft). Length: 5.10 m (16.70 ft). Country: Japan.
Engine Model: TT-210. Designer: NASDA. Gross Mass: 200 kg (440 lb). Propellants: Solid. Diameter: 0.21 m (0.68 ft). Length: 5.30 m (17.30 ft). Country: Japan.
S-210 used on Rocket Stages - Used on stage: S-210. on launch vehicle: S.
- Used on stage: TT-200. on launch vehicle: S.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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