Development Program for An Advanced In-Line Reusable Launch Vehicle Concept Using a Small-scale End-Burning Solid and Hybrid Rocket Glider Demonstrator Approach
Abstract:This paper describes a development program for assessing and demonstrating technology required for an advanced in-line reusable vehicle concept which involves use of a frozen monolithic propellant as a load bearing member and phase-change in flight in an end-consuming manner. Relative motion between a forward crew/payload module and an aft/propulsion module allows for the ability to eliminate staging requirements on ascent and allows for the ability to reuse/return main-stage engines in an attempt to significa… Show more
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