References
- Webster, F.F., "Liquid Fueled Integral Rocket Ramjet Technology Review," 14th AIAA/SAE Joint Propulsion Conference, Las Vegas, N.V., U.S.A., AIAA 1978-1108, Jul. 1978.
- Webster, F.F., "Integral Rocket/Ramjet Propulsion-Flight Data Correlation and Analysis Techniques," Journal of Spacecraft, Vol. 19, No. 4, pp. 326-336, 1981.
- Ronald S.F., "A Century of Ramjet Propulsion Technology Evolution," Journal of Propulsion and Power, Vol. 20, No. 1, pp. 27-28, 2004. https://doi.org/10.2514/1.9178
- Sung, H.G. and Yoon, H.G., "Technical Review and Analysis of Ramjet/Scramjet Technology. I. Ramjet Engine(Liquid Ramjet, Ducted Rocket)," Journal of the Korean Society of Propulsion Engineers, Vol. 10, No. 1, pp. 72-86, 2006.
- Albert, L., "Nozzleless Booster Hardware Demonstration Progress to Date," 24th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Boston, M.A., U.S.A., AIAA 1988-3366, Jul. 1988.
- Procinsky, I.M. and McHale, C.A., "Nozzleless Boosters for Integral-Rocket-Ramjet Missile Systems," Journal of Spacecraft, Vol. 18, No. 3, pp. 193-199, 1981. https://doi.org/10.2514/3.57804
- Procinsky, I.M. and Yezzi, C.A., "Nozzleless Performance Program," 18th Joint Propulsion Conference, Cleveland, O.H., U.S.A., AIAA-82-1198, Jun. 1982.
- Farinaccio, R. and Lessard, R., "Nozzleless Booster Performance Study", Technical Report, DREV TR 2001-285, 2011.
- Farinaccio, R. and Lessard, R., "Experimental Investigation of High Burn Rate Propellant for use in Nozzleless Boosters", 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Huntsville, A.L., U.S.A., AIAA 2000-3320, Jul. 2010.
- Nahon S., "Nozzleless Solid Propellant Rocket Motors Experimental and Theoretical Investigations", 20th Joint Propulsion Conference, Cincinnati, O.H., U.S.A., AIAA-84-1312, Jun. 1984.
- Krishnan, S. and Ramakrishnan, R., "Effect of Motor Length and Propellant Formulation on Nozzleless Solid Rocket Performance," Proceedings of the Institution of Mechanical Engineers, Vol. 213, No. 1, pp. 35-44, 1999. https://doi.org/10.1243/0954410991532828
- Calzone, R.F., Mayer, A.E.H.J., Dijkstra, F., Elands, P.J.M., Stowe, R.A., Farinaccio, R., Dubois, C., Lesage, F., Wong, F.C, Lessard, P. and Lauzon, M., "Integral Rocket Ramjet Demonstration Program(IRRDP) Executive Summary Report," TNO report, PML 1998-A85, 1998.
- Khil, T., Jung, E., Lee, K., Ryu, T. and Lee, H., "Development of Nozzleless Booster casted to Solid Propellant with Al as a Metal Fuel," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 4, pp. 52-62, 2017. https://doi.org/10.6108/KSPE.2017.21.4.052
- Mcbride, B.C. and Gordon, S., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, II: User Manual and Program Description," NASA RP-1311, 1996.
- Min, B.S. and Hyun, H.S., "Study on Combusiton Characteristics of HTPB/AP Propellants Containing Zirconium," Journal of Propulsion and Power, Vol. 28, No. 1, pp. 211-213, 2012. https://doi.org/10.2514/1.B34120
- Traineau, J.C. and Kuentzmann, P., "Some Measurements of Solid Propellant Burning Rates in Nozzleless Motors," J20th Joint Propulsion Conference, Cincinnati, O.H., U.S.A., AIAA-84-1469, Jun. 1984.
- Blomshield, F.S., "Lessons Learned in Solid Rocket Combustion Instability," AIAA, Missile Sciences Conference, Monterey, C.A., U.S.A., AIAA 2007-5803, Nov. 2006.
- Min, B.S, Hyun, H.S., and Yim, Y.J., "Combustion Characteristics of HTPB/AP/Zr Propellant," Journal of the Korean Society of Propulsion Engineers, Vol. 9, No. 2, pp. 9-16, 2005.
- Gany A. and Aharon I., "Internal Ballistics Condiserations of Nozzleless Rocket Motors", Journal of Propulsion and Power, Vol. 15, No. 6, pp. 866-873, 1999. https://doi.org/10.2514/2.5509