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Altitude testing of large liquid propellant engines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Maynard, Bryon Raines, Nickey |
| Copyright Year | 2008 |
| Description | Altitude Testing of the J2-X engine at 100,000 feet (start capability). Chemical Steam Generation for providing vacuum. Project Started Mar 07. Test Stand Activation around Late 2010. J-2X Testing around early 2011. |
| File Size | 3365721 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080032764 |
| Archival Resource Key | ark:/13960/t9t200660 |
| Language | English |
| Publisher Date | 2008-06-23 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Vacuum Engine Design Test Stands Liquid Rocket Propellants Steam Liquid Propellant Rocket Engines Altitude J-2 Engine Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |