Ariel 2
![]() Ariel 2 before launch | |
Names | Ariel2, S 52, S 52A, UK 2, UK-C |
---|---|
Mission type | Radio astronomy |
Operator | SERC / NASA |
COSPAR ID | 1964-015A |
SATCAT no. | 771 |
Spacecraft properties | |
Manufacturer | Westinghouse Electric |
Launch mass | 68 kilograms (150 lb) |
Start of mission | |
Launch date | 27 March 1964, 17:25:23 | UTC
Rocket | Scout X-3 |
Launch site | Wallops Island LA-3 |
Contractor | NASA |
End of mission | |
Last contact | November 1964 |
Decay date | 18 November 1967 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Eccentricity | 0.0733267483 |
Perigee altitude | 289 kilometres (180 mi) |
Apogee altitude | 1,343 kilometres (835 mi) |
Inclination | 51.6 degrees |
Period | 101.21 minutes |
Epoch | 3 May 1964[1] |
Ariel 2, also known as UK-C, was a British radio astronomy
Launch and mission parameters

The launch of Ariel 2 was conducted by the United States
Contributions to galactic radio astronomy
One of the major scientific focuses of the Ariel 2 mission was to characterize galactic radio emissions at frequencies below 10 MHz. Such frequencies are difficult to observe from Earth due to the influence of the ionosphere.[8]
It was known that a non-directional antenna operating at frequencies below 10 MHz would be sensitive to galactic radio sources, with only a small contribution due to other sources.[8] The Ariel 2 satellite had a 40m non-directional antenna that was essentially a long wire that was unreeled from a drum in the satellite after being placed into orbit.[8] In order to remove the effects of Earth-based radio waves, the antenna was tuned to detect frequencies between 0.7 and 3.5 MHz. This choice was not arbitrary. The ionosphere effectively blocks radio waves below 4 MHz. This is both a problem for Earth-bound radioastronomers (who cannot observe radio waves below 4 MHz) and a benefit for space-based observatories (which are not subject to noise at frequencies above 4 MHz).[8]
The observations were processed to determine the mean sky brightness in Ariel 2's preferred frequency band.
Telemetry and data storage/transmission
Ariel 2 could transmit data at 55 samples per second when in range of a ground station. Data transmitted in this way included operating voltages and engineering data as well as science data. Due to the need to share the channel between multiple experiments and the engineering data itself, different data were allocated different sample rates. For example, the galactic radio astronomy data was sampled at a rate of 1 sample every 75ms during times when the high-speed transmission was possible.[8]
In addition, the satellite had an on-board tape recorder, which was shared between experiments. The tape recorder was only able to sample at 1 sample per second.[8] The tape recorder data was downloaded using the high speed transmission channel when the satellite was in range of a ground station.
See also
References
- ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 6 December 2013.
- ^ Wade, Mark. "Ariel". Encyclopedia Astronautica. Archived from the original on 20 May 2002. Retrieved 7 September 2009.
- ^ "Design of a Spacecraft". Flight International. 21 January 1965. p. 115.
- ^ Krebs, Gunter. "Ariel 1, 2". Gunter's Space Page. Retrieved 7 September 2009.
- ^ "World Civil Satellites 1957-2006". Space Security Index. Archived from the original on 18 July 2011. Retrieved 7 September 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 7 September 2009.
- ^ "Traditional Micro-satellites list: 1957-1969". Surrey Satellite Technology Ltd. Archived from the original on 5 June 2009. Retrieved 7 September 2009.
- ^ .
External links
- Achieving Ariel II Design Compatibility (NASA)
- Ariel II Engineering Data Analysis Phase I Report, Volume 1
- Ariel II Engineering Data Analysis Phase I Report, Volume 2
- Ariel II Engineering Data Analysis Phase II Report
- Ariel II Engineering Data Analysis Phase III (Final) Report
- UK-2, the Second Anglo-American Satellite