35th Joint Propulsion Conference and Exhibit 1999
DOI: 10.2514/6.1999-2730
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An air-breathing launch vehicle concept for single-stage-to-orbit

Abstract: The "Trailblazer" is a 300-1b payload, single-stageto-orbit launch vehicle concept that uses air-breathing propulsion to reduce the required propellant fraction.

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Cited by 26 publications
(14 citation statements)
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“…In order to reduce space launch costs, reusable launch vehicles with short turn-around times including very robust single-stage-to-orbit (SSTO) concepts are being considered. NASA Glenn Research Center (NASA-GRC) has undertaken a program to develop such an SSTO vehicle under the concept GTX (formerly Trailblazer) [1] (see Fig. 1) which is to be powered by a rocket-based combined cycle (RBCC) engine.…”
Section: Introductionmentioning
confidence: 99%
“…In order to reduce space launch costs, reusable launch vehicles with short turn-around times including very robust single-stage-to-orbit (SSTO) concepts are being considered. NASA Glenn Research Center (NASA-GRC) has undertaken a program to develop such an SSTO vehicle under the concept GTX (formerly Trailblazer) [1] (see Fig. 1) which is to be powered by a rocket-based combined cycle (RBCC) engine.…”
Section: Introductionmentioning
confidence: 99%
“…This mechanism for flowpath destabilization is initiated before the combustor becomes thermally choked at the exit plane. This technology is currently being applied to the GTX rocket-based combined-cycle engine [16] under development at NASA Glenn Research Center. Research will be focused toward examining the dynamic response of the engine flowfield during mode transition.…”
Section: Project 2: Hypersonic Engine Component Interactionsmentioning
confidence: 99%
“…In the Independent Ramjet Stream (IRS) cycle, the design uses a different engine configuration to ensure complete mixing between injected fuel and air stream without increasing the duct length as shown in Figure 4c. This design is used by the GTX vehicle concept study by NASA [5]. Upstream of the rocket exhaust, fuel is injected into the air stream and ignites when it reaches the hot exhaust gases from the rocket.…”
Section: Figure 3: Typical Rbcc Layout With Centralized Rocketmentioning
confidence: 99%
“…The increase in mass flow augments the achievable thrust. Another study by Trefny [5], looks into single stage to orbit options and considers a RBCC engine as its primary propulsion unit.…”
Section: Introduction 11 Brief History Of Trans-atmospheric Vehicle mentioning
confidence: 99%
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