The Microwave Anisotropy Probe (MAP), a MIDEX mission built in partnership between Princeton University and the NASA Goddard Space Flight Center (GSFC), will study the cosmic microwave background. It will be inserted into a highly elliptical earth orbit for several weeks and then use a lunar gravity assist to orbit around the second Lagrangian point (L2), 1.5 million kilometers, anti-sunward from the earth. The charging environment for the phasing loops and at L2 was evaluated. There is a limited set of data for L2; the GEOTAIL spacecraft measured relatively low spacecraft potentials (approx. 50 V maximum) near L2. The main area of concern for charging on the MAP spacecraft is the well-established threat posed by the 'geosynchronous region' between 6-10 Re. The launch in the autumn of 2000 will coincide with the falling of the solar maximum, a period when the likelihood of a substorm is higher than usual. The likelihood of a substorm at that time has been roughly estimated to be on the order of 20% for a typical MAP mission profile. Because of the possibility of spacecraft charging, a requirement for conductive spacecraft surfaces was established early in the program. Subsequent NASCAP/GEO analyses for the MAP spacecraft demonstrated that a significant portion of the sunlit surface (solar cell cover glass and sunshade) could have nonconductive surfaces without significantly raising differential charging. The need for conductive materials on surfaces continually in eclipse has also been reinforced by NASCAP analyses.
Spacecraft Charging and the Microwave Anisotropy Probe Spacecraft
1998
2 pages
Report
No indication
English
Unmanned Spacecraft , Manned Spacecraft , Spacecraft charging , Microwave probes , Anisotropy , Solar storms , Radiation effects , Radiation shielding , Solar activity effects , Magnetic storms , Lunar gravitation , Geomagnetic tail , Elliptical orbits , Earth orbits , Lagrangian equilibrium points , Background radiation
TIBKAT | 2011
|NTRS | 1989
|NTIS | 1989
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