Solid rocket stage. 13.00 kN (2,923 lbf) thrust. Mass 400 kg (882 lb).
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Gross mass: 400 kg (880 lb).
Unfuelled mass: 111 kg (244 lb).
Height: 2.70 m (8.80 ft).
Diameter: 0.35 m (1.14 ft).
Thrust: 13.00 kN (2,922 lbf).
Burn time: 32 s.
Number: 288 .
Orion Aerojet solid rocket engine. 13 kN. Improved Orion motor was a bi-phase propellant system with thrust levels of 84.5 kN during the first four seconds of motor burn, trailing off to 13.3 kN at burnout at 25 seconds. More...
Associated Launch Vehicles
Orion Sounding Rocket American sounding rocket. The Orion was a single stage, unguided, fin stabilized rocket system which used a surplus US Army Hawk surface-to-air-missile rocket motor having a dual thrust propellant grain. Three fins on the aft end of the motor were canted to roll the vehicle at four revolutions per second at burnout for stability. Improved performance could be obtained by using a Nike booster stage. Payload 38 kg to 88 km or 68 kg to 71 km. More...
Nike Orion American sounding rocket. Two stage vehicle. Payload 68 kg to 190 km or 204 kg to 90 km. The Nike motor had three equally spaced unmodified Ajax fins, and the Orion motor had four fins on the aft end arranged in a cruciform configuration to provide stability. The first stage Nike booster had an action time of 3.2 seconds. The second stage ignited 9 seconds after liftoff and had an action time of 32 seconds. Capability 68 kg payload to 190 kilometers or a 204 kg payload to 90 kilometers when launched from sea level at an 85 degree launch angle. More...
Taurus Orion American sounding rocket. 2 stage vehicle composed of 1 x Taurus (Honest John motor) + 1 x Orion. Payload 68 kg to 260 km or 227 kg to 140 km. More...
HJ Orion American sounding rocket. Two stage vehicle consisting of 1 x M-6 + 1 x Orion More...
Terrier Orion American two-stage, spin-stabilized sounding rocket. It used a Terrier Mk 12 Mod 1 engine for its first stage and an improved Orion motor for its second stage. The Terrier-Orion could loft payloads weighing up to 290 kilograms to altitudes up to 190 kilometers. More...
VS-30/Orion Brazilian sounding rocket. Two stage vehicle consisting of 1 x Sonda 3-1 + 1 x Orion More...
Associated Manufacturers and Agencies
Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. More...
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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