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Scout X-2

Scout X-2 was an American expendable launch system and sounding rocket which was flown twice in 1962. It was a four-stage rocket, based on the earlier Scout X-1, uprated first and third stages. It was a member of the Scout family of rockets.

ManufacturerVought
Country of originUnited States
Size
Height25 metres (82 ft)
Diameter1.01 metres (3 ft 4 in)
Mass16,440 kilograms (36,240 lb)
StagesFour
Capacity
Payload to LEO
Mass76 kilograms (168 lb)
Associated rockets
FamilyScout
Launch history
StatusRetired
Launch sitesWallops LA-3
Point Arguello LC-D
Total launches2
Success(es)1
Failure(s)1
First flight1962-03-29
Last flight1962-04-26
First stage – Algol 1D
Powered by1 solid
Maximum thrust440 kilonewtons (99,000 lbf)
Burn time44 seconds
PropellantSolid
Second stage – Castor 1A
Powered by1 solid
Maximum thrust286 kilonewtons (64,000 lbf)
Specific impulse247 sec
Burn time27 seconds
PropellantSolid
Third stage – Antares 2A
Powered by1 X-254
Maximum thrust93 kilonewtons (21,000 lbf)
Specific impulse293 sec
Burn time36 seconds
PropellantSolid
Fourth stage – Altair 1A
Powered by1 X-248A
Maximum thrust14 kilonewtons (3,100 lbf)
Specific impulse255 sec
Burn time40 seconds
PropellantSolid

The Scout X-2 used an Algol 1D first stage, instead of the earlier Algol 1B used on the Scout X-1. The third stage was the Antares 2A, a more powerful version of the Antares 1A used on earlier variants of the Scout rocket. The second and fourth stages were the same as those used on the Scout X-1; a Castor 1A and an Altair 1A respectively.

The first Scout X-2 was launched on a suborbital flight at 07:27 GMT on 29 March 1962. It flew from Launch Area 3 of the Wallops Flight Facility. The flight carried plasma and aeronomy experiments to an apogee of 6,291 kilometres (3,909 mi), and was successful. The second flight, launched on 26 April, carried the Solrad 4B satellite. It failed to reach orbit. Following this launch, the Scout X-2 was replaced by the upgraded Scout X-2M.

References

  • Wade, Mark. . Encyclopedia Astronautica. Archived from the original on September 17, 2008. Retrieved 2009-07-03.
  • Krebs, Gunter. "Scout". Gunter's Space Page. Retrieved 2009-07-03.
  • McDowell, Jonathan. "Scout". Orbital & Suborbital Launch Database. Jonathan's Space Page. Retrieved 2009-07-03.
  • Heyman, Jos; Parsch, Andreas (2007-07-09). "LTV SLV-1 Scout". Appendix 3: Space Vehicles. Directory of U.S. Military Rockets and Missiles. Retrieved 2009-07-03.


scout, american, expendable, launch, system, sounding, rocket, which, flown, twice, 1962, four, stage, rocket, based, earlier, scout, uprated, first, third, stages, member, scout, family, rockets, manufacturervoughtcountry, originunited, statessizeheight25, me. Scout X 2 was an American expendable launch system and sounding rocket which was flown twice in 1962 It was a four stage rocket based on the earlier Scout X 1 uprated first and third stages It was a member of the Scout family of rockets ManufacturerVoughtCountry of originUnited StatesSizeHeight25 metres 82 ft Diameter1 01 metres 3 ft 4 in Mass16 440 kilograms 36 240 lb StagesFourCapacityPayload to LEOMass76 kilograms 168 lb Associated rocketsFamilyScoutLaunch historyStatusRetiredLaunch sitesWallops LA 3Point Arguello LC DTotal launches2Success es 1Failure s 1First flight1962 03 29Last flight1962 04 26First stage Algol 1DPowered by1 solidMaximum thrust440 kilonewtons 99 000 lbf Burn time44 secondsPropellantSolidSecond stage Castor 1APowered by1 solidMaximum thrust286 kilonewtons 64 000 lbf Specific impulse247 secBurn time27 secondsPropellantSolidThird stage Antares 2APowered by1 X 254Maximum thrust93 kilonewtons 21 000 lbf Specific impulse293 secBurn time36 secondsPropellantSolidFourth stage Altair 1APowered by1 X 248AMaximum thrust14 kilonewtons 3 100 lbf Specific impulse255 secBurn time40 secondsPropellantSolid edit on Wikidata The Scout X 2 used an Algol 1D first stage instead of the earlier Algol 1B used on the Scout X 1 The third stage was the Antares 2A a more powerful version of the Antares 1A used on earlier variants of the Scout rocket The second and fourth stages were the same as those used on the Scout X 1 a Castor 1A and an Altair 1A respectively The first Scout X 2 was launched on a suborbital flight at 07 27 GMT on 29 March 1962 It flew from Launch Area 3 of the Wallops Flight Facility The flight carried plasma and aeronomy experiments to an apogee of 6 291 kilometres 3 909 mi and was successful The second flight launched on 26 April carried the Solrad 4B satellite It failed to reach orbit Following this launch the Scout X 2 was replaced by the upgraded Scout X 2M References EditWade Mark Scout Encyclopedia Astronautica Archived from the original on September 17 2008 Retrieved 2009 07 03 Krebs Gunter Scout Gunter s Space Page Retrieved 2009 07 03 McDowell Jonathan Scout Orbital amp Suborbital Launch Database Jonathan s Space Page Retrieved 2009 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 Retrieved 2009 07 03 This rocketry article is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title Scout X 2 amp oldid 1120093176, wikipedia, wiki, book, books, library,

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