Predicted thermal response of a cryogenic fuel tank exposed to simulated aerodynamic heating profiles with different cryogens and fill levels
By: Gregory J. Hanna, Craig A. Stephens.
Contributors: Stephens, Craig A. 1963-; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA contractor report -- 4395.; NASA contractor report -- NASA CR-4395.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; National Technical Information Service, distributor]
Published: 1991
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic heating.; Cryogenic fluid storage.; Cryogenic fluids.; Cryogenics.; Evaporation.; Fuel tanks.; Heat flux.; Temperature effects.; Venting.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-0798-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1  microfiche.