Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines.
[Part] 2,
Hydrazine /
by Vearl N. Huff and Sandford Gordon.
APA Citation
Huff, V. N., Gordon, S., Lewis Flight Propulsion Laboratory. (1952). Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines. Washington, D.C.: National Advisory Committee for Aeronautics.
MLA Citation
Huff, Vearl N, Sanford Gordon, and Lewis Flight Propulsion Laboratory. Theoretical Performance of Liquid Ammonia, Hydrazine And Mixture of Liquid Ammonia And Hydrazine As Fuels With Liquid Oxygen Bifluoride As Oxidant for Rocket Engines. Washington, D.C.: National Advisory Committee for Aeronautics, 1952.
Warning: These citations may not always be complete (especially for serials).