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Spacecraft dielectric material properties and spacecraft charging

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Xehetasun bibliografikoak
Erakunde egilea:	ebrary, Inc
Beste egile batzuk:	Frederickson, A. R.
Formatua:	Baliabide elektronikoa eBook
Hizkuntza:	ingelesa
Argitaratua:	New York, N.Y. : American Institute of Aeronautics and Astronautics, Inc., c1986.
Saila:	Progress in astronautics and aeronautics ; v. 107.
Gaiak:	Space vehicles > Electrostatic charging. Space vehicles > Materials. Dielectrics. Electronic books.
Sarrera elektronikoa:	An electronic book accessible through the World Wide Web; click to view
Etiketak:	Etiketa erantsi Etiketarik gabe, Izan zaitez lehena erregistro honi etiketa jartzen!

Antzeko izenburuak

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Guide to mitigating spacecraft charging effects
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Spacecraft propulsion
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Elements of spacecraft design
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Spacecraft maximum allowable concentrations for selected airborne contaminants.
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Thermal design principles of spacecraft and entry bodies
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Spacecraft water exposure guidelines for selected contaminants.
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Spacecraft water exposure guidelines for selected contaminants.
Argitaratua: (2004)

Spacecraft water exposure guidelines for selected contaminants.
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Thermophysics applications to thermal design of spacecraft /
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Methods for developing spacecraft water exposure guidelines
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The space environment and its effects on space systems
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Space vehicle dynamics and control
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Pioneer Venus case study in spacecraft design
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Priorities in space science enabled by nuclear power and propulsion
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Planetary landers and entry probes
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Thermal design of aeroassisted orbital transfer vehicles
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Introduction to aerospace materials /
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Advanced power sources for space missions
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Aerospace thermal structures and materials for a new era
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Heat transfer and spacecraft thermal control Technical papers selected from the AIAA 8th Aerospace Sciences Meeting, January 1970, and the AIAA 5th Thermophysics Conference, June-July 1970, subsequently rev. for this vol /
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