Sung et al., 2003 - Google Patents
A subscale-based life prediction methodology for rocket engine combustorSung et al., 2003
- Document ID
- 15185912360706500842
- Author
- Sung I
- Northcutt B
- Rubel K
- Anderson W
- Publication year
- Publication venue
- 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
External Links
Snippet
ABSTRACT α= Thermal expansion coefficient, µm/mK δ= Kronecker delta function ε= Strain A small scale experimental annular plug nozzle thruster was designed, built and tested to failure. The test article was a water-cooled, 200 psia combustor that used decomposed …
- 238000000034 method 0 title description 7
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/56—Control
- F02K9/58—Propellant feed valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Eiringhaus et al. | Numerical investigation of a 7-element GOX/GCH4 subscale combustion chamber | |
| Pizzarelli | An algebraic model for structural and life analysis of regeneratively-cooled thrust chambers | |
| Vorobyev et al. | Thermal state calculation of chamber in small thrust liquid rocket engine for steady state pulsed mode | |
| Knab et al. | Advanced cooling circuit layout for the vinci expander cycle thrust chamber | |
| Yamanishi et al. | Transient analysis of the LE-7A rocket engine using the rocket engine dynamic simulator (REDS) | |
| Daimon et al. | Numerical and experimental investigation of the methane film cooling in subscale combustion chamber | |
| Ricci et al. | Experimental investigation on the transcritical behaviour of methane and numerical rebuilding activity in the frame of the HYPROB-BREAD Project | |
| Sung et al. | A subscale-based life prediction methodology for rocket engine combustor | |
| Boysan | Analysis of regenerative cooling ın liquid propellant rocket engines | |
| Paxson et al. | Performance impact of deflagration to detonation transition enhancing obstacles | |
| Bartolome Calvo et al. | Numerical simulation of liquid rocket engine cooling channels | |
| Battista et al. | Modelling, Testing and Design Considerations of a GOX/GCH4 Igniter for a HYPROB-SSBB Single Injector Thrust Chamber | |
| Sung et al. | A subscale-based rocket combustor life prediction methodology | |
| Kamps et al. | Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4 | |
| Babu et al. | Fatigue life prediction of a rocket combustion chamber | |
| Alanyalioglu et al. | Fully transient conjugate analysis of silica-phenolic charring ablation coupled with interior ballistics | |
| Ajmani et al. | Numerical and experimental studies of a film cooled pulsed detonation tube | |
| Anderson et al. | Rocket combustor experiments and analyses | |
| Cheng et al. | Development of GOX/kerosene swirl-coaxial injector technology | |
| Mehta et al. | Space Launch System Core-Stage Rocket Engine Development for Shock-Tunnel Testing | |
| Melle et al. | Development and test firing of a one-piece additively manufactured liquid rocket engine | |
| Betti | Flow Field and Heat Transfer Analysis of Oxygen/Methane Liquid Rocket Engine Thrust Chambers | |
| Bouchez et al. | PTAH-SOCAR Fuel-Cooled Composite Materials Structure: 2011 Status | |
| Bulman et al. | Simulated LOX-augmented nuclear thermal rocket (LANTR) testing | |
| Eiringhaus et al. | 3D conjugate heat transfer analysis of a 100 kN class liquid rocket combustion chamber |