Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute /
by Anthony Fortine and Vearl N. Huff.

Description

Main Author

Fortine, Anthony.

Related Names

Huff, Vearl N.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1957.

Subjects

Rockets (Aeronautics) > Rockets (Aeronautics) / Fuel > Rockets (Aeronautics) / Fuel / Testing.

Note

"January 25, 1957."
Cover title.

Physical Description

38, [2] p. : ill. ; 28 cm.

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