Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles by Joseph M. Roche

Cover of: Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles | Joseph M. Roche

Published by National Aeronautics and Space Administration, Glenn Research Center, National Technical Information Service, distributor in [Cleveland, Ohio], Springfield, VA .

Written in English

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Other titlesPreliminary sizing of vertical take off rocket-based combined-cycle powered launch vehicles.
StatementJoseph M. Roche, David R. McCurdy.
Series[NASA technical memorandum] -- NASA/TM-2001-210668., NASA technical memorandum -- 210668.
ContributionsMcCurdy, David R., NASA Glenn Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL17601374M
OCLC/WorldCa47948855

Download Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles

PRELIMINARY SIZING OF VERTICAL TAKE-OFF ROCKET-BASED COMBINED-CYCLE POWERED LAUNCH VEHICLES Joseph M. Roche and David R. McCurdy National Aeronautics and Space Administration Glenn Research Center Cleveland, Ohio SUMMARY The task of single-stage-to-orbit has been an elusive goal due to propulsion performance, materials limi­.

Download Citation | Preliminary Sizing of Vertical Take-Off Rocket-Based Combined-Cycle Powered Launch Vehicles | The task of single-stage-to.

Get this from a library. Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles. [Joseph M Roche; David R McCurdy; NASA Glenn Research Center.].

Multidisciplinary design of a rocket-based combined cycle SSTO launch vehicle using Taguchi methods. Combined Cycle SSTO Launch Vehicle. horizontal take-off. Introduction. A rocket-based combined-cycle (RBCC) engine exploits the synergistic interactions between a rocket and an air-breathing engine, effectively integrating a high thrust-to-weight ratio with a high specific impulse.It can function over an extensive Mach number range, and provide better performance than any single existing engine by: rocket-based combined cycle (RBCC} engine.

RBCC engines exhibit a high potential for lowering the operating cost of launching payloads into orbit. Tv,o sources of cost reductions can be identified. First, RBCC powered vehicles require only' 20% takeoff thrust compared to conventional rockets, thereby lowering the thrustFile Size: 3MB.

The space plane would use a combined cycle engine that would allow it to take off from an airport runway and fly into orbit. The rocket-based combined-cycle engine (RBCC). Launch vehicles. NOTICE TEXT: NASA/MSFC plans to issue a Request for Quotation (RFQ) for the Development of a Horizontal Take-Off and Landing (HTHL) Rocket-Based Combined Cycle (RBCC) Single Stage-to-Orbit (SSTO.

Escher, W.J.D. (a) “Rocket-Based Combined Cycle (RBCC) Powered Spaceliner Class Vehicles Can Advantageously Employ Vertical Takeoff and Landing (VTOL)”, Paper AIAApresented at the AIAA Aerospace Sciences Meeting, Reno NV, January Google ScholarAuthor: Paul A.

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A virtual encyclopedia of engineering, it is known for its completeness, easy-to-read style, and real-world approach to the process of design. The X is also fabricated from materials and construction techniques that are equivalent to the full scale operational vehicles so that operational data can be applied to a full scale Reusable Launch Vehicle (RLV) such a Venture by: 3.

vehicle can get to orbit. Also, larger vehicles can bear the weight of the NTR system much better than a smaller vehicle, but this results in a higher-powered nuclear reactor. ETO missions require a high T/W in rocket mode to reach orbit. This leads to the high reactor powers and high T/W e requirements for vehicles that can get any payloads.

Full text of "DTIC ADA A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs" See other formats. Full text of "NASA Technical Reports Server (NTRS) The Tenth Thermal and Fluids Analysis Workshop" See other formats.

Rocket Based Combined Cycle (RBCC) Engine. NASA Technical Reports Server (NTRS) Pictured is an artist's concept of the Rocket Based Combined Cycle (RBCC. Share what you know and love through presentations, infographics, documents and more.

heat exchange and pressure drop enhanced by violent sloshing (english) nasa ares i launch vehicle first stage roll control system cold flow development test program overview. experimental studies of the unsteady ejector mode of a pulse detonation rocket-based combined cycle engine.

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Dual-mode scramjets combine subsonic combustion with supersonic combustion for operation at lower speeds, and rocket-based combined cycle (RBCC) engines supplement a traditional rocket's propulsion with a scramjet, allowing for additional oxidizer to 5/5(2).

The program's major investment is in hypersonic airbreathing propulsion since it offers the greatest potential for meeting the third generation launch vehicles. The program will mature the technologies in three key propulsion areas, scramjets, rocket-based combined cycle and turbine-based combination cycle.

go back to reference Escher, W.J.D. (a) “Rocket-Based Combined Cycle (RBCC) Powered Spaceliner Class Vehicles Can Advantageously Employ Vertical Takeoff and Landing (VTOL)”, Paper AIAApresented at the AIAA Aerospace Sciences Meeting, Reno.

The Case for Space Solar Power VIRGINIA ED This book may not be reproduced, in whole or in part, without the written permission of the publisher, except for the purpose of reviews. The Expendable Launch Vehicles (ELVs) available today (c.

) deliver hardware at costs between $10, and $20, per pound. Fortunately, most of. Combined Cycle to Mach The lower map in the figure is for a combined cycle rocket ejector ram-scramjet engine powering a VTOHL SSTO (airbreather). Similar to the rocket, the available solution space lies in a narrower band between 0 tons payload at = and 10 tons payload at a range of = to Propulsion systems generally fall into two categories: Rocket-based and turbine-based.

Both approaches use dual-mode scramjets over much of the flight envelope, from Mach 3 or 4 to Mach 12 to Rocket based combined cycle (RBCC) systems use rockets in the scramjet duct for low speed acceleration and/or orbital insertion.

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RT Dissertation/Thesis, Unpublished SR 00 ID / A1 Abbruzzese, Gennaro T1 Unstructured Grid Generation Using Overset. Looking to the future, an innovative air- breathing vehicle concept was designed by Astrox, ASC/XR, AFRL, and Boeing to be the reusable second stage of a two-stage-to- orbit launch system boosted by a reusable rocket first stage.

The second stage is pow- ered by rocket-based combined-cycle (RBCC) engines fueled by methane and LOX/hydro- gen. The International Space Station would have an orbital lifetime of only a few years without the periodic orbital boosts provided by the space shuttle or other rocket-powered space vehicles such as the Russian Progress.

Most LEO satellites spend up .

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