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J-1 F2
Part of J-1
J-1 F2
J-1 F2
Japanese all-solid orbital launch vehicle. Lower cost alternate to the original J-1 design. Uses the SRB-A of the H-2A vehicle as the first stage, the second and third stages of the J-1, with updated avionics.

Status: In development. Payload: 850 kg (1,870 lb). Thrust: 1,800.00 kN (404,600 lbf). Gross mass: 91,500 kg (201,700 lb). Height: 26.20 m (85.90 ft). Diameter: 2.50 m (8.20 ft). Apogee: 250 km (150 mi).

LEO Payload: 850 kg (1,870 lb) to a 250 km orbit at 30.00 degrees. Payload: 600 kg (1,320 lb) to a 407 km 51.6 deg orbit.

Stage Data - J-1 F2



Family: all-solid, orbital launch vehicle. Country: Japan. Stages: M-23-J, M-3B-Mu, SRB-A. Agency: Nissan.

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