Manufacturer | Vought |
---|---|
Country of origin | United States |
Size | |
Height | 22 metres (72 ft) |
Diameter | 1.02 metres (3 ft 4 in) |
Mass | 17,000 kilograms (37,000 lb) |
Stages | Four |
Associated rockets | |
Family | Scout |
Launch history | |
Status | Retired |
Launch sites | Point ArguelloLC-D |
Total launches | 1 |
Failure(s) | 1 |
UTC date of spacecraft launch | 1963-09-27 |
First stage –Algol 1D | |
Powered by | 1solid |
Maximum thrust | 440 kilonewtons (99,000 lbf) |
Burn time | 44 seconds |
Propellant | Solid |
Second stage –Castor 1A | |
Powered by | 1solid |
Maximum thrust | 286 kilonewtons (64,000 lbf) |
Specific impulse | 247 sec |
Burn time | 27 seconds |
Propellant | Solid |
Third stage –Antares 2A | |
Powered by | 1X-254 |
Maximum thrust | 93 kilonewtons (21,000 lbf) |
Specific impulse | 293 sec |
Burn time | 36 seconds |
Propellant | Solid |
Fourth stage –Altair 2A | |
Powered by | 1X-258 |
Maximum thrust | 22 kilonewtons (4,900 lbf) |
Specific impulse | 266 sec |
Burn time | 28 seconds |
Propellant | Solid |
TheScout X-2B was an Americanexpendable launch system which was flown during 1963. It was a four-stage rocket, based on the earlierScout X-2, but with anAltair 2A fourth stage in place of theAltair 1A used on the X-2. It was a member of theScout family of rockets.
The Scout X-2 was an all-solid rocket, with anAlgol 1D first stageaCastor 1A second stage, anAntares 2A third stage, and an Altair 2A fourth stage. It made only one flight, which was launched fromLaunch Complex D atPoint Arguello, carrying aP-35 weather satellites,P35-5. The launch occurred on 27 September 1963, and failed to achieve orbit.
![]() | This rocketry article is astub. You can help Wikipedia byexpanding it. |