Loading...
Please wait, while we are loading the content...
Density and mixture fraction measurements in a go2/gh2 uni-element rocket chamber
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Santoro, R. J. Pal, S. Moser, M. D. |
| Copyright Year | 1994 |
| Description | In recent years, there has been a renewed interest in gas/gas injectors for rocket combustion. Specifically, the proposed new concept of full-flow oxygen rich preburner systems calls for the injection of both oxygen and hydrogen into the main chamber as gaseous propellants. The technology base for gas/gas injection must mature before actual booster class systems can be designed and fabricated. Since the data base for gas/gas injection is limited to studies focusing on the global parameters of small reaction engines, there is a critical need for experiment programs that emphasize studying the mixing and combustion characteristics of GO2 and GH2 propellants from a uni-element injector point of view. The experimental study of the combusting GO2/GH2 propellant combination in a uni-element rocket chamber also provides a simplified environment, in terms of both geometry and chemistry, that can be used to verify and validate computational fluid dynamic (CFD) models. |
| File Size | 338553 |
| Page Count | 5 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950002747 |
| Archival Resource Key | ark:/13960/t5dc2zh55 |
| Language | English |
| Publisher Date | 1994-11-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Oxygen Density Measurement Injectors Engine Design Computational Fluid Dynamics Hydrogen Gas-gas Interactions Propellant Chemistry Rocket Engines Gas Injection Propellant Combustion Data Bases Mixing Ratios Liquid Oxygen Thrust Chambers Dynamic Models Mathematical Models Hydrogen Oxygen Engines Fuel Injection Gaseous Rocket Propellants Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
