Encyclopedia Astronautica
NOTS-1


NOTS solid rocket engine. 53.4 kN. Out of production. Isp=204s. Used on Caleb launch vehicle. First flight 1960.

Thrust (sl): 53.400 kN (12,005 lbf). Thrust (sl): 5,441 kgf.

Status: Out of production.
Gross mass: 1,033 kg (2,277 lb).
Unfuelled mass: 194 kg (427 lb).
Diameter: 0.60 m (1.96 ft).
Thrust: 53.40 kN (12,005 lbf).
Specific impulse: 204 s.
Specific impulse sea level: 204 s.
Burn time: 34 s.
Number: 7 .

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Associated Countries
See also
Associated Launch Vehicles
  • Caleb American air-launched orbital launch vehicle. Heavily classifed project related to air-launched ASAT development. Launch tests in 1958. NOTS project staff believed they successully orbited a satellite but unconfirmed. More...

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...

Associated Stages
  • NOTS-1 Solid propellant rocket stage. Loaded/empty mass 1,033/194 kg. Thrust 53.36 kN. Vacuum specific impulse 204 seconds. More...

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