9780792370468 - the fast mission (5 Ergebnisse)
- Hardcover
Anbieter: Ria Christie Collections, Uxbridge, Vereinigtes KönigreichRia Christie Collections
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Zustand: New. In.
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Anbieter: moluna, Greven, Deutschlandmoluna
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Gebunden. Zustand: New.
- Hardcover
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Hardcover. Zustand: Brand New. 228 pages. 9.50x6.25x0.50 inches. In Stock.
- Hardcover
Anbieter: Kennys Bookstore, Olney, MD, USAKennys Bookstore
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Zustand: New. Contains discussion of the design philosophy of a breed of satellite to measure particles and fields in the magnetosphere. This resource provides documentation of the FAST satellite and instruments. It contains examples and descriptions of data gathered by its instruments. It is suitable for those working with resu…lts from this observatory. Editor(s): Pfaff, Robert F. Num Pages: 219 pages, biography. BIC Classification: PHVB; PHVJ; RBP. Category: (P) Professional & Vocational; (UP) Postgraduate, Research & Scholarly; (UU) Undergraduate. Dimension: 235 x 155 x 14. Weight in Grams: 550. . 2001. 98. Hardback. . . . . Books ship from the US and Ireland.
- Hardcover
Anbieter: AHA-BUCH GmbH, Einbeck, DeutschlandAHA-BUCH GmbH
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Buch. Zustand: Neu. Druck auf Anfrage Neuware - Printed after ordering - 1.1. MISSION BACKGROUND The scientific objective of this magnetospheric physics mission was a detailed in vestigation of the Aurora Borealis, or 'Northern Lights'. The fields experiments (electric and magnetic) were constructed by the University of Californ…ia at Berke ley (UCB), and Los Angeles (UCLA) respectively. The particles instruments were constructed by UCB and the University of New Hampshire in collaboration with Lockheed Palo Alto Research Laboratory. The instrument data processing unit was provided by UCB. The spacecraft bus, telemetry, and launch services were provided by the NASA Goddard Space Flight Center SMEX office. The science principal investigator is Dr C. W. Carlson of UCB, and the program is managed by the SMEX office. The UCB design philosophy emphasizes the demonstration of design margins set by peer review. As a result, each boom system was extensively tested at a prototype level before the flight units were manufactured. Additionally, the design, assembly and testing of each boom mechanism was conducted by a single engineer solely responsible for its success.
