The Aerobee 150A is a four-fin sounding rocket approximately 9 meters long and 38 centimeters in diameter, manufactured by [Space-General Corporation][aerojet] and first flown in February, 1960. The rocket is capable of transporting 45 to 130 kilograms payloads to high altitudes (over 200 kilometers) with a stable, near vertical trajectory. The rocket is a free-flight, fin-stabilized, tower-launched, vehicle consisting of a liquid propellant sustainer and a solid propellant booster. The rocket is rolled (spun) during flight to decrease dispersion.
Mass Breakdown
Aerobee 150A Sustainer
Name | Mass | [kg] |
Nosecone | 7 | .711 |
Minimum Payload | 45 | .359 |
Nose Extension | 6 | .35 |
Tank Shroud | 3 | .0 |
Head End Plumbing | 1 | .814 |
Tank Assembly | 74 | .156 |
Aniline/Furfuryl Alcohol Fuel | 134 | .354 |
IRFNA | 343 | .914 |
Aft Shroud | 7 | .031 |
Thrust Chamber Assembly | 14 | .56 |
Misc. (fasteners, etc.) | 5 | .625 |
Reserve Propellent | 6 | .35 |
Fins (4) | 12 | .701 |
Totals: | 662 | .925 |
2.5 KS-18,000 Booster
Name | Mass | [kg] |
Booster body and fins | 153 | .314 |
Propellent | 118 | .841 |
Totals: | 272 | .155 |