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Scout X-2B

From Wikipedia, the free encyclopedia
ManufacturerVought
Country of originUnited States
Size
Height22 metres (72 ft)
Diameter1.02 metres (3 ft 4 in)
Mass17,000 kilograms (37,000 lb)
StagesFour
Associated rockets
FamilyScout
Launch history
StatusRetired
Launch sitesPoint ArguelloLC-D
Total launches1
Failure(s)1
UTC date of spacecraft launch1963-09-27
First stage –Algol 1D
Powered by1solid
Maximum thrust440 kilonewtons (99,000 lbf)
Burn time44 seconds
PropellantSolid
Second stage –Castor 1A
Powered by1solid
Maximum thrust286 kilonewtons (64,000 lbf)
Specific impulse247 sec
Burn time27 seconds
PropellantSolid
Third stage –Antares 2A
Powered by1X-254
Maximum thrust93 kilonewtons (21,000 lbf)
Specific impulse293 sec
Burn time36 seconds
PropellantSolid
Fourth stage –Altair 2A
Powered by1X-258
Maximum thrust22 kilonewtons (4,900 lbf)
Specific impulse266 sec
Burn time28 seconds
PropellantSolid

TheScout X-2Bwas an Americanexpendable launch systemwhich was flown during 1963. It was a four-stage rocket, based on the earlierScout X-2,but with anAltair 2Afourth stage in place of theAltair 1Aused on the X-2. It was a member of theScoutfamily of rockets.

The Scout X-2 was an all-solid rocket, with anAlgol 1Dfirst stageaCastor 1Asecond stage, anAntares 2Athird stage, and an Altair 2A fourth stage. It made only one flight, which was launched fromLaunch Complex DatPoint Arguello,carrying aP-35weather satellites,P35-5.The launch occurred on 27 September 1963, and failed to achieve orbit.

References[edit]

  • Wade, Mark."Scout".Encyclopedia Astronautica.Archived fromthe originalon September 17, 2008.Retrieved2009-07-03.
  • Krebs, Gunter."Scout".Gunter's Space Page.Retrieved2009-07-03.
  • McDowell, Jonathan."Scout".Orbital & Suborbital Launch Database.Jonathan's Space Page. Archived fromthe originalon 2020-08-11.Retrieved2009-07-03.
  • Heyman, Jos; Parsch, Andreas (2007-07-09)."LTV SLV-1 Scout".Appendix 3: Space Vehicles.Directory of U.S. Military Rockets and Missiles.Retrieved2009-07-03.