Jump to content

Ariel 3

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Citation bot (talk | contribs) at 15:36, 23 April 2020 (Alter: pages. Add: jstor, doi, pages, issue, bibcode. Removed URL that duplicated unique identifier. Removed accessdate with no specified URL. Removed parameters. Formatted dashes. | You can use this bot yourself. Report bugs here. | Activated by Headbomb | via #UCB_webform). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

For the moped, see Ariel 3 (moped).
Ariel 3
Ariel 3 with its paddles in the deployed position
Mission typeAtmospheric studies
OperatorSERC / NASA
COSPAR ID1967-042A Edit this at Wikidata
SATCAT no.2773[1]
Mission duration43 months
Spacecraft properties
Launch mass89 kilograms (197 lb)
Start of mission
Launch date5 May 1967, 16:00:01 (1967-05-05UTC16:00:01Z) UTC
RocketScout A
Launch siteVandenberg SLC-5
End of mission
DisposalDecommissioned
DeactivatedSeptember 1969 (1969-10)
Decay date14 December 1970
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Eccentricity0.008
Perigee altitude496 kilometres (308 mi)
Apogee altitude599 kilometres (372 mi)
Inclination80.17 degrees
Period95.69 minutes
Epoch7 June 1967[2]
← Ariel 2
Ariel 4 →

Ariel 3 (UK 3 or United Kingdom Research Satellite 3) was a satellite in the Ariel programme, a satellite partnership between the US and UK. Three of the onboard experiments continued research from the first two missions and two experiments were designed for new research topics. It was launched from Vandenberg Air Force Base on 5 May 1967, making it the first satellite of the program to launch from the West coast. Ariel 3 was shut down in September 1969, and re-entered the Earth's atmosphere 14 December 1970.

This was the first artificial satellite designed and constructed in the United Kingdom.

Design

Development

In 1961 the UK Space Research Group accepted proposals for experiments to be carried on the third satellite of the Ariel programme. The British National Committee for Space Research selected experiments from those proposals and submitted them to NASA in 1962. The scientific objectives for the mission were selected in January 1963, and full work on the satellite began in early 1964 due to organisational and financial difficulties.[3] A total of 5 craft were constructed.[4] One prototype, two engineering models, the final satellite and a flight spare.[4] The flight spare was later used as the basis of Ariel 4.[5]

Operation

Power could be drawn from the batteries or the solar panels. The batteries were considered the least reliable component in the system so this method was devised to mitigate the issue.[6]

The spacecraft weighed 89 kilograms (197 lb).[7]

Sensors

Ariel 3 carried five experiments.[8] The experiments measured properties of the thermosphere as well as detected "terrestrial radio noise" from thunderstorms and measured large-scale galactic radio frequency noise.[8] Ariel 3 was also fitted with a series of mirrors to observe the spin of the satellite.[9]

High-speed data was transmitted continuously to the Satellite Tracking and Data Acquisition Network (STADAN). Low-speed data was recorded on tape recorders and was transmitted to ground stations in the high-speed mode when commanded.[10]

Three experiments expanded on data from the previous two missions. Two experiments collected data on naturally occurring radio noise.[8]

Mission

Launch

The launch was originally planned for Wallops; Ariel 1 and Ariel 2 had both launched on the East coast. In 1964 experimenters requested a change to the proposed orbit, from an inclination of 50–70° to 78–80° to maximize coverage at the geomagnetic latitude. This change precipitated the launch site moving to the West coast.[11]

It was launched from Vandenberg Air Force Base on 5 May 1967 aboard a Scout rocket.[12][1] This made it the first artificial satellite designed and constructed in the United Kingdom.[7]

Operations

Ariel 3 had an orbital period of approximately 95 minutes, with an apogee of 608 km and a perigee of 497 km. It initially spun at 31 rpm for stability, though by the time the Ariel 3 deorbited, it had slowed to a rate of about 1 rpm.[1]

On 24 October 1967 the tape recorder aboard Ariel 3 began to malfunction. This restricted observation to real-time operation only. Ariel 3 suffered from a significant power failure in December 1968, restricting the satellite's operation to daylight hours only. The satellite was completely shut down in September 1969. Its orbit decayed steadily until on 14 December 1970 when Ariel 3 re-entered Earth's atmosphere.[1]

See also

Notes

  1. ^ a b c d "Ariel 3". NASA Space Science Data Coordinated Archive. Retrieved 24 March 2020.
  2. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 6 December 2013.
  3. ^ Ladd & Smith 1969, p. 480.
  4. ^ a b Campbell, F. P. (December 1966). "Orbiting A High Atmosphere Experiment". Weather. 21 (12): 422–428. Bibcode:1966Wthr...21..422C. doi:10.1002/j.1477-8696.1966.tb02797.x.
  5. ^ Dalziel 1975, p. 163.
  6. ^ Sketch 1969, pp. 493–494.
  7. ^ a b Ladd & Smith 1969, p. 479.
  8. ^ a b c Ladd & Smith 1969, p. 481.
  9. ^ Dalziel 1979, p. 414.
  10. ^ Ladd & Smith 1969, p. 485.
  11. ^ Ladd & Smith 1969, pp. 482–483.
  12. ^ "'On This Day' for May 5, 1967 - First all-British satellite 'Ariel 3' launched". BBC News. 5 May 1967. Retrieved 1 January 2010.

References

Retrieved from "https://en.wikipedia.org/w/index.php?title=Ariel_3&oldid=952688983"