Solid rocket stage. 18.00 kN (4,047 lbf) thrust. Mass 30 kg (66 lb).
Status: Active.
Gross mass: 30 kg (66 lb).
Unfuelled mass: 6.00 kg (13.20 lb).
Height: 2.00 m (6.50 ft).
Diameter: 0.10 m (0.32 ft).
Thrust: 18.00 kN (4,046 lbf).
Burn time: 2.10 s.
Number: 993 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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Super Loki American sounding rocket. Larger-diameter version of single-stage Loki sounding rocket, developed originally for NASA's Marshall Spaceflight Center. More...
Associated Manufacturers and Agencies
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Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. More...
Associated Propellants
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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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