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Rocket ignition demonstrations using silane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pal, Sibtosh Kincaid, Kevin Watkins, William B. Santoro, Robert |
| Copyright Year | 1998 |
| Description | Rocket ignition demonstration tests using silane were performed at the Penn State Combustion Research Laboratory. A heat sink combustor with one injection element was used with gaseous propellants. Mixtures of silane and hydrogen were used as fuel, and oxygen was used as oxidizer. Reliable ignition was demonstrated using fuel lead and and a swirl injection element. |
| File Size | 162350 |
| Page Count | 5 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19990009078 |
| Archival Resource Key | ark:/13960/t3fz26x8h |
| Language | English |
| Publisher Date | 1998-10-14 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Silanes Rockets Propellants Hydrogen Ignition Combustion Injection Heat Sinks Gas Mixtures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
