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NOTS solid rocket engine. 63.2 kN.

Gross mass: 100 kg (220 lb).
Unfuelled mass: 27 kg (59 lb).
Height: 1.80 m (5.90 ft).
Diameter: 0.30 m (0.98 ft).
Thrust: 63.20 kN (14,208 lbf).
Burn time: 4.90 s.

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Associated Countries
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Associated Manufacturers and Agencies
  • NOTS American manufacturer of rocket engines and rockets. Naval Ordnance Test Station, China Lake, CA, USA. More...

Associated Propellants
  • Solid 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. 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...

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