Evaluation of propellant tank insulation concepts for low-thrust chemical propulsion systems

Evaluation of propellant tank insulation concepts for low-thrust chemical propulsion systems

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Bibliographic Details
Main Author:	Kramer, T. J
Corporate Authors:	Boeing Aerospace Company, Lewis Research Center
Other Authors:	Brogren, E. W, Siegel, B. L
Format:	Government Document Book
Language:	English
Published:	Cleveland, OH : Lewis Research Center, [1984]
Series:	NASA contractor report NASA CR-168320
Subjects:	Cryogenics Foam insulation Heat transfer Space propulsion

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