A Porous Plug Burner Technique for the Study of Composite Solid Propellant Deflagration on a Fundamental level and its Application to Hybrid Rocket Propulsion
- 1 January 1964
- book chapter
- Published by Elsevier
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- The measurement of temperature profiles through solid propellant flames using fine thermocouplesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
- RADIATION-INDUCED SOLID PROPELLANT DECOMPOSITIONPublished by Defense Technical Information Center (DTIC) ,1964
- The surface temperature of burning ammonium perchlorateCombustion and Flame, 1963
- SCHLIEREN AND SHADOWGRAPH STUDIES OF HYBRID BOUNDARYLAYER COMBUSTIONAIAA Journal, 1963
- SOME REMARKS ON THE THEORY OF FLAME PROPAGATIONPublished by Elsevier ,1963
- TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKETPublished by Elsevier ,1963
- ON THE ANALYSIS OF LINEAR PYROLYSIS EXPERIMENTSPublished by Elsevier ,1963
- The combustion of propellants based upon ammonium perchlorateSymposium (International) on Combustion, 1961
- A model describing combustion of solid composite propellants containing ammonium nitrateCombustion and Flame, 1959