| タイトル | Hot Fire Ignition Test with Densified Liquid Hydrogen using a RL10B-2 Cryogenic H2/O2 Rocket Engine |
| 本文（外部サイト） | http://hdl.handle.net/2060/19970026009 |
| 著者（英） | McNelis, Nancy B.; Haberbusch, Mark S. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1997-07-01 |
| 言語 | eng |
| 内容記述 | Enhancements to propellants provide an opportunity to either increase performance of an existing vehicle, or reduce the size of a new vehicle. In the late 1980's the National AeroSpace Plane (NASP) reopened the technology chapter on densified propellants, in particular hydrogen. Since that point in time the NASA Lewis Research Center (LERC) in Cleveland, Ohio has been leading the way to provide critical research on the production and transfer of densified propellants. On October 4, 1996 NASA LeRC provided another key demonstration towards the advancement of densified propellants as a viable fuel. Successful ignition of an RL10B-2 engine was achieved with near triple point liquid hydrogen. |
| NASA分類 | Propellants and Fuels |
| レポートNO | 97N25377
NASA-TM-107470
NAS 1.15:107470
AIAA Paper 97-2688
E-10758 |
| 権利 | No Copyright |
