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Advanced engine study program
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Branstrom, B. R. Galler, D. E. Denman, T. F. Black, J. R. Shied, R. A. Clark, G. L. Masters, A. I. Fierstein, A. R. |
| Copyright Year | 1993 |
| Description | A design and analysis study was conducted to provide advanced engine descriptions and parametric data for space transfer vehicles. The study was based on an advanced oxygen/hydrogen engine in the 7,500 to 50,000 lbf thrust range. Emphasis was placed on defining requirements for high-performance engines capable of achieving reliable and versatile operation in a space environment. Four variations on the expander cycle were compared, and the advantages and disadvantages of each were assessed. Parametric weight, envelope, and performance data were generated over a range of 7,500 to 50,000 lb thrust and a wide range of chamber pressure and nozzle expansion ratio. |
| File Size | 9023804 |
| Page Count | 248 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930019757 |
| Archival Resource Key | ark:/13960/t6547n167 |
| Language | English |
| Publisher Date | 1993-06-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Orbit Transfer Vehicles Exhaust Nozzles Engine Design Aerospace Environments Thrust Chamber Pressure Liquid Rocket Propellants Thrust Chambers Hydrogen Oxygen Engines Spacecraft Propulsion 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 |
