HTR (original) (raw)

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HTR

Nammo LOx/Solid hybrid rocket engine.

Thrust: 30.00 kN (6,744 lbf). Burn time: 20 s.

Subtopics

Hybrid Test Rocket American sounding rocket. Single stage vehicle.

Hybrid Test Rocket-1 LOx/Solid propellant rocket stage. Thrust 30.00 kN.

Family: Hybrid. Country: USA. Propellants: Lox/Solid. Stages: Hybrid Test Rocket-1. Agency: Nammo.

2007 May 3 - . 10:50 GMT - . Launch Site: Andoya. LV Family: HTR. Launch Vehicle: Hybrid Test Rocket.

HTR Technology test - . Nation: USA. Agency: ARR, Nammo. Apogee: 30 km (18 mi).

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