Design of a 2000 lbf LOX/LCH 4 Throttleable Rocket Engine for a Vertical Lander - ProQuest

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Design of a 2000 lbf LOX/LCH₄ Throttleable Rocket Engine for a Vertical Lander

Lopez, Israel. The University of Texas at El Paso ProQuest Dissertations Publishing, 2017. 10283859.