Cambier, 2002 - Google Patents
Mhd power generation from a pulse detonation rocket engineCambier, 2002
- Document ID
- 11169967937863567624
- Author
- Cambier J
- Publication year
- Publication venue
- 33rd Plasmadynamics and Lasers Conference
External Links
Snippet
This paper summarizes a preliminary investigation [1] of the potential for power generation from coupling a Pulse Detonation Rocket Engine (PDRE) with a MHD generator. The PDRE configuration is similar to a rocket engine, except that the operation is pulsed, and the …
- 238000005474 detonation 0 title abstract description 33
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
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
- F02K7/06—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with combustion chambers having 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
- F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/46—Feeding propellants using pumps
- F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
-
- 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
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Wu et al. | System performance and thermodynamic cycle analysis of airbreathing pulse detonation engines | |
| Bratkovich et al. | An introduction to pulse detonation rocket engines (PDREs) | |
| Talei et al. | Sound generation by laminar premixed flame annihilation | |
| Kailasanath et al. | Performance estimates of pulsed detonation engines | |
| Gray et al. | Thermodynamic evaluation of pulse detonation combustion for gas turbine power cycles | |
| Wintenberger | Application of steady and unsteady detonation waves to propulsion | |
| Cooper et al. | The effect of nozzles and extensions on detonation tube performance | |
| Nielsen | Hydrodynamic calculations of surface response in the presence of laser‐supported detonation waves | |
| Cambier | Mhd power generation from a pulse detonation rocket engine | |
| Geng et al. | Combined numerical and experimental investigation of a hobby-scale pulsejet | |
| Paulson et al. | Ideal Thermodynamic performance results for rotating detonation rocket engine thrust chambers using CEA | |
| Ross et al. | Flow acceleration in an RDRE with gradual chamber constriction | |
| Alavilli et al. | Ignition-transient modeling for solid propellant rocket motors | |
| Zhang et al. | Numerical studies of multi-cycle detonation induced by shock focusing | |
| Eidelman et al. | Pulsed detonation engine: Key issues | |
| Allgood et al. | Effects of exit geometry on the performance of a pulse detonation engine | |
| Bauer et al. | Design and test of a resonance ignition system for green in-orbit propulsion systems | |
| Zuniga | Investigation of Detonation Theory and the Continuously Rotating Detonation Engine | |
| Kailasanath et al. | On factors controlling the performance of pulsed detonation engines | |
| Knowlen et al. | Ram accelerator performance modeling | |
| He et al. | Reactive flow phenomena in pulse detonation engines | |
| Godil et al. | Numerical simulation of ignition transient in solid rocket motor: a revisit | |
| Bellini | Ideal cycle analysis of a regenerative pulse detonation engine for power production | |
| Kassoy et al. | Thermomechanical Response of Reactive Gas to Rapid Transient, Spatially Distributed Energy Addition: An Asymptotic Formulation | |
| Cambier et al. | The pulse detonation rocket induced MHD ejector (PDRIME) concept |