Open Access
Issue |
JNWPU
Volume 36, Number 3, June 2018
|
|
---|---|---|
Page(s) | 558 - 564 | |
DOI | https://doi.org/10.1051/jnwpu/20183630558 | |
Published online | 08 October 2018 |
- Hueter Uwe, Turner Jim. Rocket-Based Combined Cycle Activities in the Advanced Space Transportation Program Office[R]. AIAA-1999-2352 [Google Scholar]
- Trefny Charles J. An Air-Breathing Launch Vehicle Concept for Single-Stage-to-Orbit[R]. AIAA-1999-2730 [Google Scholar]
- Takeshi Kanda, Kenji Kudo. A Conceptual Study of a Combined Cycle Engine for an Aerospace Plane[R]. AIAA-2002-5146 [Google Scholar]
- Takeshi Kanda, Kenji Kudo. Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane[J]. Journal of Propulsion and Power, 2003, 19(5):859-867 [Article] [CrossRef] [Google Scholar]
- Takeshi Kanda, Kouichiro Tani, Kenji Kudo. Conceptual Study of a Rocket-Ramjet Combined-Cycle Engine for an Aerospace Plane[J]. Journal of Propulsion and Power, 2007, 23(2):301-309 [Article] [CrossRef] [Google Scholar]
- Lehman M, Pal S, Santoro R J. Experimental Investigation of the RBCC Rocket-Ejector Mode[R]. AIAA-2000-3725 [Google Scholar]
- Li Yufei, He Guoqiang, Liu Peijin. Experimental Study for Factors Affecting Rocket Ejector Performance in SMC Combustion Mode[J]. Journal of Propulsion Technology, 2006, 27(2):97-100 (in Chinese) [Article] [Google Scholar]
- Liu Yang, He Guoqiang, Liu Peijin, et al. Numerical and Experimental Investigation on Effect of Primary Rocket Flow on Performance of RBCC[J]. Journal of Solid Rocket Technology, 2008, 31(5):439-444 (in Chinese) [Article] [Google Scholar]
- Li Qiang, Liu Peijin, Chen Jian. Influence of Mixture Ratio of Primary Flow on Secondary Combustion Flame Stability of Ejector Rocket Motor[J]. Journal of Solid Rocket Technology, 2009, 32(4):427-430, 435 (in Chinese) [Article] [Google Scholar]
- Lü Xiang, Liu Peijin, He Guoqiang, et al. Optimization Method for Primary Rocket Mass Flow Rate in Rocket Ejector Mode[J]. Journal of Solid Rocket Technology, 2010, 33(6):631-635 (in Chinese) [Article] [NASA ADS] [Google Scholar]
- Pan Kewei, He Guoqiang, Liu Peijin, et al. Influence of Combustion Stabilization by Primary Rocket under Commix-Combustion Mode in RBCC[J]. Journal of Propulsion Technology, 2010, 31(5):544-548 (in Chinese) [Article] [Google Scholar]
- Escher W J D, Schnurstein R E. A Retrospective on Early Cryogenic Primary Rocket Subsystem Designs as Integrated into Rocket-Based Combined-Cycle(RBCC) Engines[R]. AIAA-1993-1944 [Google Scholar]
- Pryor D E, Hyde E H, Escher W J D. Development of a 12-Thrust Chamber Kerosene/Oxygen Primary Rocket Subsystem for an Early(1964) Air-Augmented Rocket Ground Test System[R]. AIAA-1999-4896 [Google Scholar]
- Miller K J, Sisco J C, Austin B L, et al. Design and Ground Testing of a Hydrogen Peroxide/Kerosene Combustor for RBCC Application[R]. AIAA-2003-4477 [Google Scholar]
- Masao Takegoshi, Sadatake Tomioka, Shuichi Ueda, et al. Firing-Tests of a Rocket Combustor for Combined Cycle Engine at Various Conditions[R]. AIAA-2005-4286 [Google Scholar]
- Masao Takegoshi, Sadatake Tomioka, Shuichi Ueda, et al. Performances of a Rocket Chamber for the Combined-Cycle Engine at Various Conditions[R]. AIAA-2006-7978 [Google Scholar]
- Masao Takegoshi, Sadatake Tomioka, Fumiei Ono, et al. Injectors and Combustion Performance of Rocket Thruster for Rocket-Ramjet Combined-Cycle Engine Model[R]. AIAA-2012-5915 [Google Scholar]
- Zhu Shaohua, Tian Liang, Li Xuan, et al. Experimental Investigations of a GO2/Kerosene Ejector Rocket Chamber for the RBCC Propulsion System[R]. AIAA-2014-3989 [Google Scholar]
- Zhu Shaohua, Tian Liang, Liu Yabing, et al. Design and Experimental Investigation of Ejector Rocket Chamber for RBCC Propulsion System[J]. Journal of Propulsion Technology, 2014, 35(10):1378-1386 [Article] [Google Scholar]
- Liu Yongxing, Wang Kui, Cao Zaiyong. Investigation of GO2/Kerosene Thrust Chamber of the Main Rocket Engine for the RBCC Propulsion System[J]. Journal of Rocket Propulsion, 2009, 35(6):23-26 [Article] [Google Scholar]
- Cheng Gary C, Davis Rory R, Johnson Curtis W, et al. Numerical Cold Flow and Combustion Characterization of Swirl Coaxial Injectors[R]. AIAA-2003-4751 [Google Scholar]
- Soller S, Wagner R, Kau H P, et al. Characterisation of Main Chamber Injectors for GOX/Kerosene in a Single Element Rocket Combustor[R]. AIAA-2005-3750 [Google Scholar]
- Gordon Sanford, Mcbride Bonnie J. Computer Program for Calculation of Complex Chemical Equilibrium Compositions and ApplicationsⅠ: Analysis[R]. NASA Reference Publication 1311, 1994 [Google Scholar]
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.