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Contents

   



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1 Spacecraft design  





2 Launch  





3 See also  





4 References  














Explorer S-56 (satellite)







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From Wikipedia, the free encyclopedia
 

(Redirected from S-56 (satellite))

Explorer S-56
The identical Explorer 9 satellite
NamesNASA S-56
Mission typeAir density research
OperatorNASA
COSPAR IDEXS-56
Mission durationFailed to orbit
Spacecraft properties
SpacecraftExplorer S-56
Spacecraft typeAir Density Explorer
BusS-56
ManufacturerLangley Research Center
Launch mass7 kg (15 lb)
Dimensions3.66 m (12.0 ft) diameter
Powersolar cells and
rechargeable batteries
Start of mission
Launch date4 December 1960,
21:14 GMT
RocketScout X-1 (ST-3)
Launch siteWallops Flight Facility, LA-3
ContractorVought
End of mission
DestroyedFailed to orbit
Orbital parameters
Reference systemGeocentric orbit (planned)
RegimeMedium Earth orbit
Perigee altitude545 km (339 mi)
Apogee altitude2,225 km (1,383 mi)
Inclination38.91°
Period118.6 minutes
Explorer Program
 

Explorer S-56 was a NASA satellite launched on 4 December 1960, at 21:14 GMT as part of the Explorer program.[1] The satellite was composed of a 3.66 m (12.0 ft) diameter inflatable sphere, and was intended to study the density of the upper atmosphere. The Scout X-1 rocket used to launch Explorer S-56 failed in flight, and the satellite never reached orbit.[2]

Spacecraft design[edit]

The spacecraft consisted of alternating layers of aluminium foil and Mylar polyester film. Uniformly distributed over the aluminium surface were 5.1 cm (2.0 in)-diameter dots of white paint for thermal control. The sphere was packed in a tube 21.6 cm (8.5 in) in diameter and 48.3 cm (19.0 in) long and mounted in the nose of the fourth stage of its Scout X-1 launch vehicle.[2]

Upon separation of the fourth stage, the sphere will be inflated by a nitrogen gas bottle, and a separation spring will eject it out into its own orbit. The two hemispheres of aluminium foil will be separated with a gap of Mylar at the spacecraft's equator and will serve as the antenna. A 136 MHz, 15 mW beacon will be carried for tracking purposes, the beacon and the SAO Baker-Nunn camera network will be relied upon for tracking. Power will be supplied by solar cells and rechargeable batteries.

Launch[edit]

Explorer S-56 was launched, at 21:14 GMT on 4 December 1960, from Launch Area 3 at the Wallops Flight Facility (WFF), atop a Scout X-1 launch vehicle with the serial number ST-3. It was the first attempt to place a satellite in orbit using an all-solid propellant launch vehicle and the first orbital attempt made from NASA's Wallops Island facility. It was the first spacecraft launched from Wallops Island, but failed to reach orbit due to the second stage not igniting and impacting in the Atlantic Ocean, at 130 km (81 mi) at east of Wallops Island.[3] It was replaced by the identical Explorer 9 (1961-004A) spacecraft.[4]

The first of six identical air density research satellites to be launched.[2]

See also[edit]

References[edit]

  1. ^ "S-56". Encyclopedia Astronautica. 2019. Archived from the original on 28 December 2016. Retrieved 3 November 2021.
  • ^ a b c "AD A, B, C / DAD B (S-56 / Explorer (9), 9, 19, 24, 39, (57))". Gunter's Space Page. 8 April 2020. Retrieved 3 November 2021.
  • ^ "Display: S-56 EXS-56". NASA. 28 October 2021. Retrieved 4 November 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  • ^ McDowell, Jonathan (21 July 2021). "Launch Catalog". Jonathan's Space Report. Retrieved 3 November 2021.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Explorer_S-56_(satellite)&oldid=1194323301"

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