Explorer 27: Difference between revisions
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A three-axis [[magnetometer]] and Sun sensors provided information on the satellite attitude and spin rate.<ref name=Combrinck>Ludwig Combrinck, 2010. Sciences of Geodesy (Cap. 9) ''Springer-Verlag'' Retrieved June 9, 2018</ref> There was no [[tape recorder]] aboard so that satellite could be received only when the satellite was within range of a ground [[telemetry]] station. Continuous [[Doppler effect|Doppler]] transmitters operated at 162 [[Hertz|MHz]] and 324-MHz to permit precise tracking by [[Transit (satellite)|Transit]] tracking stations for navigation and geodetic studies.<ref name="Display"/> Four other transmitters operated on 20, 40, 41, and 360-MHz to measure ionospheric density. Explorer 27's last experiment was an Electron Density Experiment designed for measuring charged particles in the immediate vicinity of the satellite.<ref name=envtest/> |
A three-axis [[magnetometer]] and Sun sensors provided information on the satellite attitude and spin rate.<ref name=Combrinck>Ludwig Combrinck, 2010. Sciences of Geodesy (Cap. 9) ''Springer-Verlag'' Retrieved June 9, 2018</ref> There was no [[tape recorder]] aboard so that satellite could be received only when the satellite was within range of a ground [[telemetry]] station. Continuous [[Doppler effect|Doppler]] transmitters operated at 162 [[Hertz|MHz]] and 324-MHz to permit precise tracking by [[Transit (satellite)|Transit]] tracking stations for navigation and geodetic studies.<ref name="Display"/> Four other transmitters operated on 20, 40, 41, and 360-MHz to measure ionospheric density. Explorer 27's last experiment was an Electron Density Experiment designed for measuring charged particles in the immediate vicinity of the satellite.<ref name=envtest/> |
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S-66 mounted 360 {{cvt| |
S-66 mounted 360 {{cvt|25|mm}} "cube corner" [[retroreflectors]] made of [[Fused quartz|fused silica]],<ref name=envtest/> so that the satellite could be tracked via lasers beamed from mobile stations at [[Wallops Flight Facility]] (WFF).<ref name=anda/>{{rp|346}}<ref name=philtrans>{{cite journal|date=1977|title=Goddard laser systems and their accuracies |url=https://royalsocietypublishing.org/doi/pdf/10.1098/rsta.1977.0017|journal=Philosophical Transactions of the Royal Society|volume=284|issue=1326|location=London|publisher=McGraw Hill Publishing Company |pages=443–444|doi=10.1098/rsta.1977.0017|bibcode=1977RSPTA.284..443V|access-date=October 21, 2019|last1=Vonbun|first1=F. O.|s2cid=122709982|hdl=2060/19760015443|hdl-access=free}}</ref> |
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== History == |
== History == |
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Revision as of 21:04, 8 November 2021
 Depiction of Explorer 27 in orbit | |
| Names | BE-C Beacon Explorer-C Beacon-C NASA S-66C |
|---|---|
| Mission type | Ionospheric research |
| Operator | NASA |
| COSPAR ID | 1965-032A |
| SATCAT no. | 01328 |
| Mission duration | ~8 years (achieved) |
| Spacecraft properties | |
| Bus | Beacon Explorer |
| Manufacturer | Johns Hopkins University Applied Physics Laboratory |
| Launch mass | 60.8 kg (134 lb) |
| Dimensions | 30 × 45 cm (12 × 18 in) |
| Power | 4 deployable solar arrays and batteries |
| Start of mission | |
| Launch date | 29 April 1965, 14:17:00 GMT |
| Rocket | Scout X-4 (S-136R) |
| Launch site | Wallops Flight Facility, |
| Contractor | Vought |
| Entered service | 29 April 1965 |
| End of mission | |
| Last contact | 20 July 1973 |
| Orbital parameters | |
| Reference system | Geocentric orbit |
| Regime | Low Earth orbit |
| Perigee altitude | 932.3 km (579.3 mi) |
| Apogee altitude | 1,311.3 km (814.8 mi) |
| Inclination | 41.1° |
| Period | 107.6 minutes |
| Instruments | |
| Electron Density Experiment Langmuir probe Passive laser tracking reflectors Radio Beacon | |
Explorer program | |
Explorer 27 (or BE-C or Beacon Explorer-C, Beacon-C or S-66C) was a small NASA satellite, launched in 1965, designed to conduct scientific research in the ionosphere.[1] It was powered by 4 solar panels. One goal of the mission was to study in detail the shape of the Earth by way of investigating variations in its gravitational field.[2] It was the third and last of the Beacons in the Explorers program. The satellite was shut off in July 1973 so that its transmission band could be used by higher-priority spacecraft.[1]
Spacecraft
Built at the Applied Physics Laboratory (APL),[4] under the direction of Goddard Space Flight Center,[3] Explorer 27 began as S-66C, the last of the five satellites in NASA's first stage of ionospheric exploration, and the first of five NASA geodetic satellites.[5]: 346 Its primary mission was "to conduct ionospheric measurements on a worldwide basis. The program will determine the total electron content of a vertical cross-section of the ionosphere located between the satellite and the Earth. Accomplishing this objective will aid in establishing the behavior pattern of the ionosphere as a function of latitude, time of day, season, and solar cycle".[3]
Weighing 60.8 kg (134 lb), the satellite was an octagonal spacecraft with a honeycomb nylon and fiberglass hull, 45 cm (18 in) in diameter, 30 cm (12 in) high, with four solar panels 25 cm (9.8 in) wide and 170 cm (67 in) long.[3]
A three-axis magnetometer and Sun sensors provided information on the satellite attitude and spin rate.[6] There was no tape recorder aboard so that satellite could be received only when the satellite was within range of a ground telemetry station. Continuous Doppler transmitters operated at 162 MHz and 324-MHz to permit precise tracking by Transit tracking stations for navigation and geodetic studies.[1] Four other transmitters operated on 20, 40, 41, and 360-MHz to measure ionospheric density. Explorer 27's last experiment was an Electron Density Experiment designed for measuring charged particles in the immediate vicinity of the satellite.[3]
S-66 mounted 360 25 mm (0.98 in) "cube corner" retroreflectors made of fused silica,[3] so that the satellite could be tracked via lasers beamed from mobile stations at Wallops Flight Facility (WFF).[5]: 346 [7]
History
The first S-66 was scheduled for launch in late 1963. However, due to problems with the Scout X-4,[3] the flight was rescheduled for the following year on a Delta B, from Cape Canaveral LC-17A.[8] On 19 March 1964, the first attempt to this S-66 ended in failure when the third stage of its Delta launch vehicle burned just 22 seconds instead of the programmed 40 seconds. This was only the second time the Delta launch vehicle had failed, and the incident followed 22 prior successes.[5]: 109
A second S-66 was launched, this time successfully, via a Scout X-4 launch vehicle at 03:01 GMT, on 9 October 1964, from the PALC-D launch facility at Vandenberg Air Force Base. Once in space, it became known as Explorer 22.[8] Explorer 22's as-yet unnamed backup was scheduled for launch in March/April 1965 to extend the geodetic experiments of its predecessor.[9] Upon the backup's launch on 29 April 1965 at 14:17:00 GMT via Scout X-4 from Wallops Island, this third S-66 satellite was designated Explorer 27.[8]
Results
Explorer 27 was turned off on 20 July 1973 because it was interfering with other, more important satellites. Tracking of the satellite via its passive laser reflectors continued at least into the 21st century.[10]
See also
References
- ^ a b c "Display: Explorer 27 (BE-C) 1965-032A". NASA. 28 October 2021. Retrieved 8 November 2021.
This article incorporates text from this source, which is in the public domain.
- ^ "Explorer Series of Spacecraft". NASA. Retrieved 12 April 2018.
- ^ a b c d e f g "Environmental test program of the beacon explorer spacecraft" (PDF). NASA. Retrieved 23 October 2019. Cite error: The named reference "envtest" was defined multiple times with different content (see the help page).
- ^ Brian Harvey (24 November 2017). Discovering the Cosmos with Small Spacecraft: The American Explorer Program. Springer. pp. 91–. ISBN 978-3-319-68140-5.
- ^ a b c "Astronautics and Aeronautics, 1964" (PDF). NASA. Retrieved 23 October 2019. This article incorporates text from this source, which is in the public domain.
- ^ Ludwig Combrinck, 2010. Sciences of Geodesy (Cap. 9) Springer-Verlag Retrieved June 9, 2018
- ^ Vonbun, F. O. (1977). "Goddard laser systems and their accuracies". Philosophical Transactions of the Royal Society. 284 (1326). London: McGraw Hill Publishing Company: 443–444. Bibcode:1977RSPTA.284..443V. doi:10.1098/rsta.1977.0017. hdl:2060/19760015443. S2CID 122709982. Retrieved 21 October 2019.
- ^ a b c McDowell, Jonathan (21 July 2021). "Launch Log". Jonathan's Space Report. Retrieved 8 November 2021.
- ^ "Beacon Explorer Surveys Ionosphere". Aviation Week and Space Technology. 19 October 1964. p. 35. Retrieved 21 October 2019.
{{cite magazine}}: Cite magazine requires|magazine=(help) - ^ "Beacon-C". International Laser Ranging Service. Retrieved 8 November 2021. This article incorporates text from this source, which is in the public domain.
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