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Advanced oxygen-hydrocarbon rocket engine study (Document No: 19810020618)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ewen, R. L. Mueggenburg, H. Obrien, C. J. Salkeid, R. |
| Copyright Year | 1980 |
| Description | Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were used to produce a consistent and reliable data base for vehicle optimization and design studies. cycles G and C were chosen for design analysis. Preliminary design analysis of the heat transfer subsystem was performed to establish major technology requirements. |
| File Size | 7139192 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810020618 |
| Archival Resource Key | ark:/13960/t0xq1t64b |
| Language | English |
| Publisher Date | 1980-08-11 |
| 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 ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |