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Advanced Low-Cost o₂/H₂ Engines for the SSTO Application [microform]

B. David Goracke and Daniel J.H. Levack, Robert F. Nixon
Format
Book; Government Document; Microform
Published
Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
Language
English
Variant Title
Advanced low cost O₂/H₂ engines for the SSTO application
Series
NASA-TM
NASA Technical Memorandum
SuDoc Number
NAS 1.15:111897
Description
1 v.
Notes
Shipping list no.: 97-0960-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Series Statement
NASA-TM ; 111897
NASA technical memorandum 111897
Technical Details
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  • Staff View

    LEADER 01913nam a22004937a 4500
    001 u2753763
    003 SIRSI
    005 19991027120526.0
    008 991027s1994 dcu b f000 0 eng d
    035
      
      
    a| (Sirsi) tmp97206349
    035
      
      
    a| (Sirsi) tmp97206349
    035
      
      
    a| (OCoLC)42711061
    037
      
      
    a| 19970005454 b| NASA
    040
      
      
    a| GPO c| GPO d| DLC d| MvI
    049
      
      
    a| VAMM
    074
      
      
    a| 0830-D (MF)
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    0
      
    a| NAS 1.15:111897
    100
    1
      
    a| Goracke, B. David.
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    1
    0
    a| Advanced low-cost O₂/H₂ engines for the SSTO application h| [microform] / c| B. David Goracke and Daniel J.H. Levack, Robert F. Nixon.
    246
    2
      
    a| Advanced low cost O₂/H₂ engines for the SSTO application
    260
      
      
    a| Washington, D.C. : b| American Institute of Aeronautics and Astronautics : b| [National Aeronautics and Space Administration ; a| Springfield, Va. : b| National Technical Information Service, distributor, c| 1994]
    300
      
      
    a| 1 v.
    490
    1
      
    a| NASA-TM ; v| 111897
    500
      
      
    a| Shipping list no.: 97-0960-M.
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    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, d| 1997] e| 1 microfiche.
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    a| 2
    650
      
    7
    a| Single stage to orbit vehicles. 2| nasat
    650
      
    7
    a| Thermodynamic cycles. 2| nasat
    650
      
    7
    a| Specific impulse. 2| nasat
    650
      
    7
    a| Engine design. 2| nasat
    650
      
    7
    a| Propulsion system configurations. 2| nasat
    650
      
    7
    a| Closed cycles. 2| nasat
    650
      
    7
    a| Liquid propellant rocket engines. 2| nasat
    700
    1
      
    a| Levack, Daniel J. H.
    700
    1
      
    a| Nixon, Robert F.
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    0
    a| NASA technical memorandum v| 111897.
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    a| United States. b| National Aeronautics and Space Administration.
    900
      
      
    a| tmp97206349
    999
      
      
    a| NAS 1.15:111897 w| SUDOC i| X005024601 l| 3EAST m| ALDERMAN t| MICROFICHE
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Alderman 3rd Floor East Reading Room N/A Available Non-Circ.