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

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100 1 ⊔ ‡aHuff, Vearl N.
245 1 0 ‡aTheoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines ‡n[Part] 2, ‡pHydrazine / ‡cby Vearl N. Huff and Sandford Gordon.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c[1952].
300 ⊔ ⊔ ‡a20 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNational Advisory Committee for Aeronautics research memorandum ; ‡vE52G09
500 ⊔ ⊔ ‡aOn front cover: "September 8, 1952."
500 ⊔ ⊔ ‡aTitle from cover.
504 ⊔ ⊔ ‡aIncludes bibliographical references: p. 7.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAmmonia.
650 ⊔ 0 ‡aHydrazine.
650 ⊔ 0 ‡aRocket engines.
650 ⊔ 0 ‡aAeronautics ‡xResearch.
700 1 ⊔ ‡aGordon, Sanford ‡ejoint author.
710 1 ⊔ ‡aUnited States. ‡bNational Advisory Committee for Aeronautics. ‡tNACA research memorandum.
710 2 ⊔ ‡aLewis Flight Propulsion Laboratory.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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