ISEE-2
ISEE-2 | |
Names | ISEE-2 |
---|---|
Mission type | study Earth's magnetic field and the solar wind |
Operator | NASA, ESRO (ESA) |
COSPAR ID | 1977-102A |
SATCAT № | 10423 |
Spacecraft properties | |
Launch mass | 340 kg (750 lb) |
Start of mission | |
Launch date | 13:53, October 22, 1977 --> |
Rocket | Delta |
Launch site | Cape Canaveral AFS |
End of mission | |
Decay date | September 26, 1987 |
Orbital parameters | |
Reference system | Geocentric |
Eccentricity | 0.91 |
Perigee | 1.04 Earth radii |
Apogee | 23 Earth radii |
Inclination | 28.76° |
Period | 3556.8 |
Epoch | October 22, 1977 |
The International Sun-Earth Explorer 2 (ISEE-2) was a space probe used to study magnetic fields near the Earth. ISEE-1 and ISEE-2 were launched on October 22, 1977, and they re-entered on September 26, 1987.[1][2] The instruments on board ISEE-2 were designed to measure electric and magnetic field properties.
Mission
The space probe was part of a program consisting of three spacecraft: a mother/daughter pair (ISEE-1 and ISEE-2) and the ISEE-3 spacecraft (later renamed to International Cometary Explorer). The program was a cooperative mission between NASA and ESRO (later ESA) designed to study the interaction between the Earth's magnetic field and the solar wind. At least 32 institutions were involved, and the focus was on understanding magnetic fields.[3] ISEE-1 (a.k.a. Explorer 56) and ISEE-3 were built by NASA, while ISEE-2 was built by ESA. All three had complimentary instruments supported by the same group of over 100 scientists.[3]
See also
- ISEE-1
- International Cometary Explorer
- 1977 in spaceflight
- List of heliophysics missions
- European Space Research Organisation
References
- ↑ "NASA - NSSDC - Spacecraft - Details". Nssdc.gsfc.nasa.gov. Retrieved 2014-03-12.
- ↑ "NASA - NSSDC - Spacecraft - Details". Nssdc.gsfc.nasa.gov. Retrieved 2014-03-12.
- 1 2 "ISEE - eoPortal Directory - Satellite Missions". Directory.eoportal.org. Retrieved 2014-03-12.