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X-34 main propulsion system-selected subsystem analyses
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McDonald, J. P. Champion Jr., R. H. Brown, T. M. Knight, K. C. |
| Copyright Year | 1998 |
| Description | The X-34 hypersonic flight vehicle is currently under development by Orbital Sciences Corporation (Orbital). The Main Propulsion System (MPS) has been designed around the liquid propellant Fastrac rocket engine currently under development at NASA Marshall Space Flight Center. This paper presents selected analyses of MPS subsystems and components. Topics include the integration of component and system level modeling of the LOX dump subsystem and a simple terminal bubble velocity analysis conducted to guide propellant feed line design. |
| File Size | 288184 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19990009342 |
| Archival Resource Key | ark:/13960/t4pk5b30b |
| Language | English |
| Publisher Date | 1998-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Propellants Engine Design X-34 Reusable Launch Vehicle Terminal Velocity Liquid Oxygen Liquid Propellant Rocket Engines Hypersonic Vehicles Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
