Explorer 52 / Hawkeye 1
|Mission type||Space Physics|
|Operator||NASA / LaRC|
|Website||NASA NSSDC Master Catalog|
|Mission duration||1,425 days|
|Manufacturer||Department of Physics and Astronomy, University of Iowa|
|BOL mass||22.7 kilograms (50 lb)|
|Start of mission|
|Launch date||23:09:11, June 3, 1974|
|Launch site||Vandenberg SLC-5|
|End of mission|
|Decay date||April 28, 1978|
|Perigee||469 kilometres (291 mi)|
|Apogee||125.570 kilometres (78.026 mi)|
|Inclination||89.81° to 81.85°|
|Triaxial Fluxgate Magnetometer
Low-Energy Protons and Electrons
This satellite was also known as:
- Hawkeye 1
- IE D
- Injun 6
- Injun F
- Neutral Point Explorer
The primary mission objective of Hawkeye 1 (Explorer 52) was to conduct particles and fields investigations of the polar magnetosphere of the earth out to 21 earth radii. Secondary objectives were to make magnetic field and plasma distribution measurements in the solar wind, and to study Type-3 radio emissions caused by solar electron streams in the interplanetary medium. To accomplish these objectives, the spacecraft was instrumented with following instruments:
- a plasma wave receiver,
- a fluxgate magnetometer, and
- a low energy proton-electron differential energy analyzer.
The spacecraft was spin stabilized with a nominal rotational period of 11 s. In celestial coordinates, the positive spin axis coordinates were right ascension 299.4 degrees (plus or minus 1.1 deg) and declination 8.6 deg (plus or minus 1.5 deg). There was no onboard orientation or spin rate control, but the orientation of the spin axis was stable. An optical aspect system operated from launch until September 3, 1974 at which time the optical aspect system was turned off and failed to turn back on. After this period, aspect had to be determined by observing the effect of optical illumination from the sun on a plasma measurement system. Using the sharp peak observed in this data, corrected orientation information was obtained and rewritten to the data records. The complete spacecraft with instruments had a mass of 22.65 kilograms (49.9 lb). Power of 22 to 36 W, depending on solar aspect, was obtained from solar cells. Hawkeye 1 participated in the International Magnetospheric Study (IMS) and during the first half of 1977 data acquisition was confined to IMS special intervals. Data were obtained in real time only, at frequencies of 136 and 400 MHz at 100 bit/s (or 200 bit/s with convolutional coding) plus wideband VLF data.
It was designed, built, and tracked by personnel at the Department of Physics and Astronomy, University of Iowa whose sports teams are the Hawkeyes. The spacecraft was launched on June 3, 1974 into a polar orbit with initial apogee over the North Pole and re-entered on April 28, 1978 after 667 orbits or nearly four years of continuous operation. The spacecraft apogee was between 20.28 and 20.92 Earth radii with less than a 1.7 Earth radii perigee. The orbital period was 51.3 hours. During its lifetime, the inclination of the plane of the spacecraft's orbit to the Earth's equator decreased monotonically from 89.81 to 81.85 degrees. The spacecraft's axis of rotation at launch was inertially fixed in its orbital plane, directed towards a constant right ascension and declination, and nearly parallel to the Earth's equatorial plane.
- "Scout (Algol-3 based)". Gunter's Space Page. Retrieved 22 March 2015.
- "NSSDC/COSPAR ID: 1974-040A". NSSDC Master Catalog Search. National Aeronautics and Space Administration. Retrieved 22 March 2015.
- http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1974-040A-03 ELF/VLF Receivers
- http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1974-040A-01 Triaxial Fluxgate Magnetometer
- http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1974-040A-02 Low-Energy Protons and Electrons