Turbojet accelerator for a single-stage-to-orbit vehicle
31st Joint Propulsion Conference and Exhibit ; 1995 ; San Diego , CA , U.S.A.
01.01.1995
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Optimal Design of Hypersonic Turbojet Engines for Two-Stage-to-Orbit Spaceplane
Online Contents | 2008
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