共 50 条
- [1] Ascent trajectory design method for RBCC-powered vehicle [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2010, 31 (07): : 1331 - 1337
- [2] Design Considerations of RBCC-powered Vehicle [J]. PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 1060 - 1063
- [3] Thrust Requirements for RBCC Powered Hypersonic Cruise Vehicles [J]. PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 1127 - 1130
- [4] Ascent and cruise trajectory optimization for ramjet powered missile [J]. Hangkong Dongli Xuebao/Journal of Aerospace Power, 2021, 36 (05): : 1103 - 1112
- [5] An affordable RBCC-powered 2-stage small orbital payload transportation systems concept based on test-proven hardware [J]. SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - 1998, PTS 1-3: 1ST CONF ON GLOBAL VIRTUAL PRESENCE; 1ST CONF ON ORBITAL TRANSFER VEHICLES; 2ND CONF ON APPLICAT OF THERMOPHYS IN MICROGRAV; 3RD CONF ON COMMERCIAL DEV OF SPACE; 3RD CONF ON NEXT GENERAT LAUNCH SYST; 15TH SYMP ON SPACE NUCL POWER AND PROPULSION, 1998, (420): : 999 - 1006
- [7] POWERED TRAJECTORY STUDIES FOR LOW THRUST SPACE VEHICLES [J]. ARS JOURNAL, 1961, 31 (01): : 28 - 32
- [8] Trajectory design and optimization of powered common aero vehicles [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2009, 30 (04): : 738 - 743
- [9] Boost-cruise Trajectory Optimization of Air Breathing Hypersonic Vehicles [J]. Yuhang Xuebao/Journal of Astronautics, 2021, 42 (07): : 820 - 829
- [10] RBCC constant dynamic pressure booster trajectory design and propellant mass flowrate analysis for TSTO transportation system [J]. Xue, R. (ruixue87@126.com), 1600, Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China (36):