Figures of the Article
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J58 engine[8]
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Working process of the J58 engine[9]
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Variation of installation thrust and specific impulse along the SR-71 flight trajectory[11]
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General layout of the SR-71 aircraft[12]
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Fligh envelope of the SR-71 aircraft[12]
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RTA-1 high-speed turbine engine[13]
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RTA-2 high-speed turbine engine[13]
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Thrust performance of the RTA engine[18]
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TSTO concept utilizing RTA engines in the first stage[16]
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TSTO concept utilizing combined RTA scramjet engines[16]
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HYPR90-T engine[19]
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HYPR90-C engine[20]
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Mass injection pre-compressor cooling (MIPCC) engine[23]
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Variation of the water-to-oxygen ratiowith the Mach number[24]
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SteamJet engine performance[24]
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RASCAL launch system decomposition[26]
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System diagram of the ATREX engine[27]
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Principle diagram of the PCTJ engine cycle[29]
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Performance comparison between ATREX and PCTJ engines[31] (TIT = 1200 K,
πfan=3 ,πcomp=10 ) -
Thermodynamic cycles of precooled engines with intermediate medium[34-37]
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SABRE3 engine performance[34]
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SABRE4 engine performance[36]
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System diagram of the ATR engine[41]
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ATR/Scramjet engine performance[42]
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Operating modes of the RBCC engine[46]
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RBCC engine performance[47]