TR-1-1

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TR-1-1

Solid rocket stage. 608.00 kN (136,684 lbf) thrust. Mass 10,800 kg (23,810 lb).

Status: Retired 1998. Thrust: 608.00 kN (136,683 lbf). Gross mass: 10,800 kg (23,800 lb). Unfuelled mass: 3,900 kg (8,500 lb). Burn time: 51 s. Height: 7.10 m (23.20 ft). Diameter: 1.10 m (3.60 ft).

Subtopics

TR-1A-1 Solid rocket stage. 608.00 kN (136,684 lbf) thrust. Mass 7,500 kg (16,535 lb).

TR-1-10800 NASDA solid rocket engine.

TR-1-7500 NASDA solid rocket engine.

Country: Japan. Launch Vehicles: TR-1. Propellants: Solid. Agency: NASDA.

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