Encyclopedia Astronautica
HTR

Nammo Lox/Solid hybrid rocket engine. 30 kN.

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

Associated Countries

See also

Associated Manufacturers and Agencies

Nammo Norwegian manufacturer of rocket engines and rockets. Nammo Raufoss AS, Norway. More...

Associated Propellants

Lox/Solid Liquid oxygen was the earliest, cheapest, safest, and eventually the preferred oxidiser for large space launchers. Its main drawback is that it is moderately cryogenic, and therefore not suitable for military uses where storage of the fuelled missile and quick launch are required. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

Associated Stages

Hybrid Test Rocket-1 Lox/Solid propellant rocket stage. Loaded mass 500 kg. Thrust 30.00 kN. More...