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Explorer 9

From Wikipedia, the free encyclopedia
NASA satellite of the Explorer program

Explorer 9
Explorer 9 before launch
NamesS-56A
Explorer IX
NASA S-56A
Mission typeAir density research
OperatorNASA
Harvard designation1961 Delta 1
COSPAR ID1961-004AEdit this at Wikidata
SATCATno.00081
Mission duration3 years (achieved)
Spacecraft properties
SpacecraftExplorer IX
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 date16 February 1961,
13:05:00GMT
RocketScout X-1 (ST-4)
Launch siteWallops Flight Facility,LA-3
ContractorVought
Entered service16 February 1961
End of mission
Decay date9 April 1964
Orbital parameters
Reference systemGeocentric orbit[1]
RegimeMedium Earth orbit
Perigee altitude545 km (339 mi)
Apogee altitude2,225 km (1,383 mi)
Inclination38.91°
Period118.6 minutes
Instruments
Satellite Drag Atmospheric Density
Explorer Program

Explorer 9, known asS-56A before launch, was aNASA satellite which was launched in February 1961 to study the density and composition of the upperthermosphere and lowerexosphere.[2] It was a reflight of the failedExplorer S-56 mission, and consisted of a 7 kg (15 lb), 3.66 m (12.0 ft)balloon which was deployed into amedium Earth orbit.[3] The mission was conducted byNASA'sLangley Research Center.

Spacecraft

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The spacecraft consisted of alternating layers ofaluminium foil andMylarpolyester 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 itsScout X-1 launch vehicle.[4]

Experiment

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Satellite Drag Atmospheric Density

[edit]

Because of its symmetrical shape, Explorer 9 was selected for use in determining upper atmospheric densities as a function of altitude, latitude, season, and solar activity. Density values near perigee were deduced from sequential observations of the spacecraft position, using optical (Baker-Nunn camera network) and radar tracking techniques. A good discussion of the general techniques used to deduce density values from satellite drag data can be found in L. G. Jacchia and J. Slowey, "Accurate drag determination for eight artificial satellites of atmospheric densities and temperatures",Smithsonian Astrophysical Observatory special report n. 100,Cambridge, Massachusetts, July 1962.[5] This experiment resulted in the successful determination of reasonable density values until the satellite reentered the Earth's atmosphere on 9 April 1964.[6]

Launch

[edit]
Launch of Explorer 9 on a Scout X-1 (ST-4) on 16 February 1961.

Explorer 9 was launched fromLaunch Area 3 at theWallops Flight Facility (WFF), atop aScout X-1 launch vehicle with the serial number ST-4. It was the first spacecraft launched from Wallops Island to achieve orbit, with one previous attempt having failed. The launch occurred at 13:05:00 GMT on 16 February 1961, and resulted in Explorer 9 being deployed into an orbit with anapogee of 2,225 km (1,383 mi), aperigee of 545 km (339 mi), 38.91° ofinclination and aperiod of 118.6 minutes.[7] It was assigned theHarvard designation 1961 Delta 1.[8]

Upon separation of the fourth stage, the sphere was inflated by anitrogen gas bottle, and a separation spring ejected it out into its own orbit. The two hemispheres of aluminium foil were separated with a gap of Mylar at the spacecraft's equator and served as the antenna. A 136 MHz, 15 mWbeacon was carried for tracking purposes, but the beacon failed on the first orbit and the SAOBaker-Nunn camera network had to be relied upon for tracking. Power was supplied bysolar cells andrechargeable batteries.[1]

The second of six identicalair density research satellites to be launched, Explorer 9 was the first to successfully reach orbit. It was still operational when the next satellite in the series,Explorer 19, was launched, allowing simultaneous readings to be taken and compared.[4]

Mission results

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Careful and continuous photographic observation of the satellite allowed scientists to conduct an unprecedented survey of the Earth'sexosphere. The satellite first confirmed the daily bulge in theupper atmosphere caused by the Sun's heating the air during the day and verified the model of exospheric temperature developed according to other satellite data.[9] It was later discovered that the temperature of the exosphere increased after geomagnetic disturbances in theionosphere, peaking around five hours after each event.[10] With three years of data, scientists were able to discern a seasonal variation to theexosphere's density, with an increase of 25% observed in winter over summer at a referencelatitude of 39°. The delay in the temperature increase resulting from magnetic disturbances was further refined to 5.2 ± 0.4 hours.[11]

Explorer 9 was the first spacecraft placed in orbit by an all-solid launch vehicle and the first spacecraft successfully launched into orbit from Wallops Island. The spacecraft reentered the Earth's atmosphere on 9 April 1964.[1]

Legacy

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A replica of the spacecraft, possibly a flight backup, is currently located in theSmithsonian Institution'sNational Air and Space Museum, although it is not on display.[12]

See also

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References

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  1. ^abc"Display: Explorer-9 1961-004A". NASA. 28 October 2021. Retrieved3 November 2021.Public Domain This article incorporates text from this source, which is in thepublic domain.
  2. ^Smith, Woody."Explorer Spacecraft Series". NASA. Retrieved17 June 2010.Public Domain This article incorporates text from this source, which is in thepublic domain.
  3. ^Wade, Mark."S-56". Encyclopedia Astronautica. Archived fromthe original on 28 October 2002. Retrieved17 June 2010.
  4. ^abKrebs, Gunter (8 April 2020)."AD A, B, C / (S-56) / Explorer S-56, 9, 19, 24, 39, 57". Gunter's Space Page. Retrieved7 November 2021.
  5. ^Jacchia, Luigi G.; Slowey, Jack (1963)."Accurate drag determinations for eight artificial satellites: atmospheric densities and temperatures".Smithsonian Contributions to Astrophysics.8 (1):1–99.doi:10.5479/si.00810231.8-1.1.hdl:10088/6623.ISSN 0081-0231.
  6. ^"Experiment: Satellite Drag Atmospheric Density". NASA. 28 October 2021. Retrieved3 November 2021.Public Domain This article incorporates text from this source, which is in thepublic domain.
  7. ^McDowell, Jonathan."Satellite Catalog". Jonathan's Space Report. Retrieved17 June 2010.
  8. ^McDowell, Jonathan (21 July 2021)."Launch Log". Jonathan's Space Report. Retrieved3 November 2021.
  9. ^Jacchia, L. G.; Slowey, J. (1962)."Preliminary Analysis of the Atmospheric Drag of the Twelve-Foot Balloon Satellite (1961 δ1)".Sao Special Report.84.Bibcode:1962SAOSR..84.....J. Retrieved21 December 2018.
  10. ^"Analysis of the Atmospheric Drag of the Explorer IX satellite from Precisely Reduced Photographic Observations". Retrieved21 December 2018.
  11. ^Roemer, M. (1966)."Atmospheric Densities and Temperatures from Precisely Reduced Observations of the Explorer IX Satellite".Sao Special Report.199.Bibcode:1966SAOSR.199.....R. Retrieved21 December 2018.
  12. ^"Satellite, Explorer 9, Balloon Replica". National Air and Space Museum. Archived fromthe original on 22 December 2018. Retrieved21 December 2018.
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