NDLI: Advanced oxygen-hydrocarbon rocket engine study (Document No: 19810014651)

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Advanced oxygen-hydrocarbon rocket engine study (Document No: 19810014651)

Content Provider	NASA Technical Reports Server (NTRS)
Author	Kent, S. Ewen, R. L. Obrien, J. O. Meagher, G. M.
Copyright Year	1980
Description	The program consists of parametric analysis and design to provide a consistent engine system data base for defining advantages and disadvantages, system performance and operating limits, engine parametric data, and technology requirements for candidate high pressure LO2/Hydrocarbon engine systems. The parametric chamber and nozzle cooling analysis was completed for the four potential coolants: RP-1, LCH4, LO2, and LH2. A summary of the cooling capability of each propellant is presented.
File Size	1963488
Page Count	53
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19810014651
Archival Resource Key	ark:/13960/t9j43k73c
Language	English
Publisher Date	1980-04-10
Access Restriction	Open
Subject Keyword	Spacecraft Propulsion And Power Orbit Transfer Vehicles Propulsive Efficiency Space Shuttle Boosters Data Bases Tables Data Systems Engineering Liquid Oxygen Hydrocarbon Fuels Oxygen-hydrocarbon Rocket Engines Liquid Propellant Rocket Engines Booster Rocket Engines Rocket Engine Design Graphs Charts Cryogenic Rocket Propellants Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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