Open Access
| Issue |
Volume 11, 2019
Progress in Propulsion Physics – Volume 11
|
|
|---|---|---|
| Page(s) | 699 - 712 | |
| DOI | https://doi.org/10.1051/eucass/201911699 | |
| Published online | 08 February 2019 | |
- Schöttle, U. M., H. Grallert, and F. A. Hewitt. 1989. Advanced air-breathing propulsion concepts for winged launch vehicles. Acta Astronaut. 20:117–129. [NASA ADS] [CrossRef] [Google Scholar]
- Schade, C., and M. Mosier. 1994. The Pegasus launch vehicle: New capabilities and the future. AIAA Paper No. 1994-1172. [Google Scholar]
- Socher, A., and A. Gany. 2008. Investigation of combined air-breathing/rocket propulsion for air launch of microsatellites from a combat aircraft. AIAA Paper No. 2008-5003. [Google Scholar]
- Heiser, W. H., D. T. Pratt, D. D. Daley, and U. B. Mehta. 1994. Hypersonic air-breathing propulsion. AIAA education ser. Washington, DC: AIAA. 594 p. [Google Scholar]
- King, M. K. 1982. Ignition and combustion of boron particles and clouds. J. Space-craft Rockets 19(4):294–306. [NASA ADS] [CrossRef] [Google Scholar]
- Kubota, N., and T. Kuwahara. 1991. Combustion of energetic fuel for ducted rockets (i). Propell. Explos. Pyrot. 16(2):51–54. [Google Scholar]
- Limage, C. R. 1996. Solid fuel ducted rockets for ramjet/scramjet missile applications. AIAA Paper No. 1996-2916. [Google Scholar]
- Kubota, N. 2007. Ducted rocket propulsion. Propellants and explosives: Thermo-chemical aspects of combustion. 2nd ed. Tokio, Japan: John Wiley & Sons. Ch. 15. P. 439–468. [Google Scholar]
- Besser, H. L. 2008. History of ducted rocket development at Bayern-Chemie. AIAA Paper No. 2008-5261. [Google Scholar]
- Gordon, S., and B. McBride. 1996. Computer program for calculation of complex chemical equilibrium compositions and applications. NASA RP 1311. [Google Scholar]
- Military specification. 1973. Engine, aircraft, turbojet and turbofan, general specification for. MIL-E-5007D. Military Specifications and Standards. DOD, USA. [Google Scholar]
- Perut, C. 1993. Propellants for integral rocket ramjet systems. Solid rocket propulsion technology. Ed. A. Davenas. 1st ed. Tarry-town, NY, USA: Pergamon Press. Ch. 12. 525–552. [Google Scholar]
- Nanda, J. K., and P. A. Ramakrishna. 2013. Development of AP/HTPB based fuel rich propellant for solid propellant ramjet. AIAA Paper No. 2013-4171. [Google Scholar]
- Hall, K. P., E. K. Bastress, and M. Summerfield. 1961. Burning rate control factors in solid propellants. 10th Quarterly Technical Summary Report. Department of the Navy, Occe of Naval Research, DTIC No.A952071. [Google Scholar]
- Cohen, N. S. 1983. A pocket model for aluminum agglomeration in composite propellants. AIAA J. 21(5):720–725. [NASA ADS] [CrossRef] [Google Scholar]
- Maggi, F., L. T. DeLuca, and A. Bandera. 2015. Pocket model for aluminum agglomeration based on propellant microstructure. AIAA J. 53(11):3395–3403. [NASA ADS] [CrossRef] [Google Scholar]