Title :
The AMPTE IRM Spacecraft
Author :
Hausler, B. ; Melzner, F. ; Stöcker, J. ; Valenzuela, A. ; Bauer, O.H. ; Parigger, P. ; Sigritz, K. ; Schoning, R. ; Seidenschwang, E. ; Eberl, F. ; Kaiser, K.-H. ; Lieb, W. ; Merz, B. ; Pagel, U. ; Wiezorrek, E. ; Genzel, J.P.
Author_Institution :
Max-Planck-Institut fÿr ex traterrestrische Physik, Garching, Germany
fDate :
5/1/1985 12:00:00 AM
Abstract :
The AMPTE Ion Release Module (IRM) together with the other two AMPTE spacecraft, UKS and CCE, were successfully launched with a Delta 3924 vehicle on August 16, 1984 from Cape Canaveral, Florida. The IRM satellite was designed, built, and tested by the Max-Planck-Institut fÿr extraterrestrische Physik. It carries 16 barium and lithium release containers and a plasna diagnostic instrument set. This paper discusses the requirements imposed on the spacecraft design by the mission and the scientific instruments and gives a description of the major spacecraft systems. Finally, a short summary of the first events in the mission is presented.
Keywords :
Artificial satellites; Barium; Instruments; Lithium; Power generation; Solar power generation; Space vehicles; Telecommunications; Telemetry; Testing;
Journal_Title :
Geoscience and Remote Sensing, IEEE Transactions on
DOI :
10.1109/TGRS.1985.289513