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151017s2000 xx o 000 0 eng d |
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|a EBLCP
|b eng
|e pn
|c EBLCP
|d OCLCQ
|d MERUC
|d OCLCQ
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|a 9781600862564
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|a 160086256X
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|a DEBBG
|b BV044094860
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|a (OCoLC)922978810
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|a TL783.4 ǂb A77 1960eb
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|a 629.4222
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|a UAMI
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|a Bollinger, Loren E.
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|a Liquid Rockets And Propellants.
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| 260 |
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|a Reston :
|b American Institute of Aeronautics and Astronautics,
|c 2000.
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| 300 |
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|a 1 online resource (698 pages)
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a Print version record.
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|a ""Cover""; ""Title""; ""Copyright""; ""Liquid Rockets Committee and Propellants and Combustion Committee""; ""Contributors to Volume 2""; ""Preface""; ""Contents""; ""A. Simulated High-Altitude Testing of Rockets""; ""Experimental Investigation of Exhaust Diffusers for Rocket Engines""; ""Summary of Experience in the Use of Exhaust Diffusers for Rocket Testing""; ""Short Diffuser for Testing Rocket Nozzles""; ""A Large Rocket Ejector System""; ""Development of an Exhaust Diffuser for Ground Testing Rocket Engines""; ""B. Instrumentation for Combustion Instability""
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| 505 |
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|a ""Instrumentation for Research on Combustion Instability in Solid-Propellant Rocket Motors""""Some Instrumentation for Combustion Stability Research""; ""An Integrated Combustion Instability Recording and Analysis Installation""; ""High Frequency Pressure Instrumentation for Rocket Instability Studies""; ""Instrumentation for Studies of Unstable Burning Phenomena""; ""C. Liquid Propellant Combustion""; ""Monodisperse Spray Deflagration""; ""A Two-Wavelength Interferometric Technique for the Study of Vaporization and Combustion of Fuels""
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| 505 |
8 |
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|a ""An Experimental Study of RP-1, UDMH and N[sub(2)]H[sub(4)] Single-Droplet Burning in Air and in Oxygen""""D. Reaction Kinetics""; ""The Reaction of Diborane and Oxygen under Explosive and Pre-Explosive Conditions""; ""Consideration of Hydrazine Decomposition""; ""Detonability of Ozone and Nitric Oxide""; ""Nonequilibrium Chemical Recombination Effects in Exhaust Nozzle Flow: An Approximate Method""; ""Spectroscopic Techniques for the Determination of Flame Temperatures: Total Radiation Techniques""; ""Production and Properties of Liquid Ozone and Liquid Ozone-Oxygen Mixtures, A Review""
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| 505 |
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|a ""E. Propellant Selection""""Liquid Propellant Comparison Based on Vehicle Performance""; ""Comparative Applicability of Storable Propellants: Effects of Specific Impulse and Density""; ""F. Rocket Engine Design""; ""Investigation of a Gas-Driven Jet Pump for Rocket Engines""; ""Analysis of Pressure Feasibility Limits in Regenerative Cooling of Combustion Chambers for Large-Thrust Rockets""; ""Fabrication, Structural and Heat Transfer Considerations of Electroformed Rocket Nozzles""; ""Design of Catalyst Packs for the Decomposition of Hydrogen Peroxide""; ""Variable Thrust Rocket Engines""
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| 500 |
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|a ""Starting Transients of Hypergolic Bipropellant Rockets""""Analysis of a New Concept Rocket Nozzle""
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| 590 |
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
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| 650 |
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0 |
|a Liquid propellant rockets
|v Congresses.
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| 650 |
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6 |
|a Fusées à propergol liquide
|v Congrès.
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| 650 |
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7 |
|a Liquid propellant rockets
|2 fast
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| 655 |
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7 |
|a Conference papers and proceedings
|2 fast
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| 700 |
1 |
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|a Goldsmith, Martin.
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| 700 |
1 |
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|a Lemmon, Alexis W.
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| 758 |
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|i has work:
|a Liquid Rocket and Propellants (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCY67yQtbwBKyTFJwtwW8kC
|4 https://id.oclc.org/worldcat/ontology/hasWork
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| 776 |
0 |
8 |
|i Print version:
|a Bollinger, Loren E.
|t Liquid Rockets And Propellants.
|d Reston : American Institute of Aeronautics and Astronautics, ©2000
|z 9781563478512
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| 856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111553
|z Texto completo
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| 938 |
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|a ProQuest Ebook Central
|b EBLB
|n EBL3111553
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| 994 |
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|a 92
|b IZTAP
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