Ariel 5

Summary

Ariel 5 (or UK 5) was a joint British and American space telescope dedicated to observing the sky in the X-ray band. It was launched on 15 October 1974 from the San Marco platform in the Indian Ocean and operated until 1980. It was the penultimate satellite to be launched as part of the Ariel programme.

Ariel 5
Mission typeAstronomy
OperatorSERC / NASA
COSPAR ID1974-077A Edit this at Wikidata
SATCAT no.7471
Spacecraft properties
ManufacturerGoddard Space Flight Center
Launch mass130.5 kg (288 lb)
Start of mission
Launch date15 October 1974, 07:47:00 (1974-10-15UTC07:47Z) UTC
RocketScout B-1
Launch siteSan Marco
End of mission
Decay date14 March 1980
Orbital parameters
Eccentricity0.00325
Perigee altitude512 km (318 mi)
Apogee altitude557 km (346 mi)
Inclination2.9 degrees
Period95.3 minutes
Epoch14 October 1974, 23:00:00 UTC[1]
Instruments
  • Rotation Modulation Collimator
  • 2- to 10-KeV Sky Survey Instrument
  • High-Resolution Source Spectra
  • Bragg Crystal Spectrometer
  • High-Energy Cosmic X-Ray Spectra
  • All-Sky Monitor
← Ariel 4
Ariel 6 →
 

Background edit

Ariel 5 was the fifth and penultimate satellite of the joint British and American Ariel programme.[2] It was the third satellite in the series built entirely in the UK.[3] It was named UK 5 before launch and renamed to Ariel 5 after the successful launch.[4]

Plans for Ariel 5 were first discussed between the UK and US in May 1967 at the Ariel 3 launch. The Science Research Council (SRC) advertised a request for proposal for experiments in June. Experiments were formally proposed to NASA in July 1968.[5]

Satellite design edit

Development edit

Marconi Space and Defence Systems (MSDS) in Portsmouth was selected as the prime contractor in 1969. SRC had them select MSDS Frimley for the attitude control system (ACS) and MSDS Stanmore for the core stores.[4]

A study was performed to see if the Scout rocket's heat shield could be enlarged to accommodate larger experiments for this mission. A larger heat shield was designed which allowed for a US experiment and five British experiments.[4]

Operation edit

Ariel 5 was spin-stabilized.[3] The satellite improved on the attitude control of Ariel 4.[6] It used liquid propane that was expanded through a reducing valve and heated with the bulk tank temperature.[7]

Power was derived from solar cells that were mounted to 7/8 of the circumference of the spacecraft. It was stored in a 3.0 Ah Ni-Cd battery.[7]

Sensors edit

The all-sky monitor (ASM) was two one-dimensional pinhole cameras scanned most of the sky every spacecraft revolution.[8] The angular resolution was 10° × 10°, with an effective area of 3 cm2 (0.465 sq in), and a bandpass of 3–6 keV. The ASM was designed to fit a resource budget of 2 kg (4.4 lb), 1 bit per second, and 1 W.[8]

The sky survey instrument (SSI) had an angular resolution of 0.75 × 10.6°, with an effective area of 290 cm2 (45 sq in), and a bandpass of 2–20 keV.[8]

Mission edit

Launch edit

Launch operations took six weeks, starting from the time the Guppy took off from Thorney Island.[9] The satellite was launched on 15 October 1974 from the San Marco platform in the Indian Ocean off the coast of Kenya.[10]

Operations edit

The satellite was controlled via a mission control centre in Appleton Lab.[11] It spun at over 10 revolutions/minute.[11] Ariel 5 operated until 1980.[2]

Results edit

Over 100 scientific papers were published within four years of the launch.[12]

Notes edit

  1. ^ "Ariel 5 Trajectory Details". NASA Space Science Data Coordinated Archive. Retrieved 8 March 2020.
  2. ^ a b "HEASARC: Observatories - The Ariel V Satellite". NASA. Archived from the original on 27 December 2013. Retrieved 3 March 2008.
  3. ^ a b Krebs, Gunter. "Ariel 5 (UK 5)". Gunter's Space Page. Retrieved 8 March 2020.
  4. ^ a b c Smith & Courtier 1976, p. 422.
  5. ^ Smith & Courtier 1976, p. 421.
  6. ^ Dalziel 1979, p. 413.
  7. ^ a b Smith & Courtier 1976, p. 429.
  8. ^ a b c Priedhorsky WC; Holt SS (1987). "Long-term cycles in cosmic X-ray sources". Space Sci Rev. 45 (3–4): 291–348. Bibcode:1987SSRv...45..291P. doi:10.1007/BF00171997. S2CID 120443194.
  9. ^ Smith & Courtier 1976, p. 428.
  10. ^ "Cooperative Space Mission Provides New Knowledge". Grand Prairie Daily News. Grand Prairie, Texas. 18 October 1974. p. 8 – via Newspapers.com.
  11. ^ a b "Ariel 5". NASA Space Science Data Coordinated Archive. Retrieved 9 March 2020.
  12. ^ Harvey 2003, p. 99.

References edit

  • Dalziel, R. (2–6 July 1979). The Significance of UK Spacecraft Control to Space Science. Automatic Control in Space: 8th IFAC Symposium. Oxford, England. ISBN 9781483158976.
  • Harvey, Brian (2003). Europe's Space Programme: To Ariane and Beyond. Springer. ISBN 9781852337223.
  • Smith, J.F.; Courtier, G.M. (1 October 1976). "The Ariel 5 Programme". Proceedings of the Royal Society of London. Mathematical and Physical Sciences. Great Britain. 350 (1663): 421–439. Bibcode:1976RSPSA.350..421S. doi:10.1098/rspa.1976.0115. JSTOR 78979. S2CID 128761336.

Further reading edit

  • Sanford, P. W.; Ives, J. C. (1976). "Ariel Results on Extragalactic X-Ray Sources". Proceedings of the Royal Society of London. Series A, Mathematical and Physical Sciences. 350 (1663): 491–503. Bibcode:1976RSPSA.350..491S. doi:10.1098/rspa.1976.0120. ISSN 0080-4630. JSTOR 78984. S2CID 83270830.