Solid rocket stage. 102.00 kN (22,931 lbf) thrust. Mass 1,200 kg (2,646 lb).
Status: Active.
Gross mass: 1,200 kg (2,600 lb).
Unfuelled mass: 341 kg (751 lb).
Height: 3.30 m (10.80 ft).
Diameter: 0.56 m (1.83 ft).
Thrust: 102.00 kN (22,930 lbf).
Burn time: 20 s.
Number: 46 .
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Associated Countries
Associated Engines
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S-30 IAE solid rocket engine. 20.490 kN. Development ended 1997. Isp=275s. More...
Associated Launch Vehicles
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Sonda 3 Brazilian sounding rocket. Two stage vehicle consisting of 1 x Sonda 3-1 + 1 x Sonda 2A More...
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Sonda 3 M1 Brazilian sounding rocket. Two stage vehicle consisting of 1 x Sonda 3-1 + 1 x Sonda 2M More...
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Sonda 4 Brazilian sounding rocket. Two stage vehicle consisting of 1 x S-43 + 1 x Sonda 3-1 More...
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VS-30 Brazilian sounding rocket. Single stage suborbital launch vehicle. More...
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VS-30/Orion Brazilian sounding rocket. Two stage vehicle consisting of 1 x Sonda 3-1 + 1 x Orion More...
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VSB-30 Brazilian two stage sounding rocket consisting of 1 x S-31 plus 1 x S-30. It replaced the British Skylark for suborbital flights from Kiruna. More...
Associated Manufacturers and Agencies
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IAE Brazilian agency overseeing development of rocket engines. Instituto de Aeronautica e Espace, Brazil. 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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