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Filters: Keyword is separable part of a rocket; deceleration detonation propulsion system; deceleration detonation propulsion design scheme; the arithmetic progression method; specific thrust impulse and Author is O.S. Aksyonov  [Clear All Filters]
2021
1Zolotko OE, 1Zolotko OV, 1Sosnovska OV, 1Aksyonov OS, 1Savchenko IS. Tte stage deorbiting with a deceleration pulse detonation engine. Space Science and Technology. 2021 ;27(4):32-41.