Operation Of A Cryogenic Rocket Engine

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Operation Of A Cryogenic Rocket Engine

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Author : Wolfgang Kitsche
language : en
Publisher: Springer Science & Business Media
Release Date : 2010-11-03

Operation Of A Cryogenic Rocket Engine written by Wolfgang Kitsche and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2010-11-03 with Technology & Engineering categories.

This book presents the operational aspects of the rocket engine on a test facility. It will be useful to engineers and scientists who are in touch with the test facility. To aerospace students it shall provide an insight of the job on the test facility. And to interested readers it shall provide an impression of this thrilling area of aerospace.

Operation Of A Cryogenic Rocket Engine

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Author :
language : en
Publisher: Springer
Release Date : 2011-04-11

Operation Of A Cryogenic Rocket Engine written by and has been published by Springer this book supported file pdf, txt, epub, kindle and other format this book has been release on 2011-04-11 with categories.

Two Phase Flow In Cryogenic Rocket Engine Feed Systems

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Author : M. Popp
language : en
Publisher:
Release Date : 1989

Two Phase Flow In Cryogenic Rocket Engine Feed Systems written by M. Popp and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with categories.

Design Of Liquid Propellant Rocket Engines

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Author : Dieter K. Huzel
language : en
Publisher:
Release Date : 1971

Design Of Liquid Propellant Rocket Engines written by Dieter K. Huzel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Liquid propellant rocket engines categories.

Technology Developments For Cryogenic Rocket Engines

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Author : H. Immich
language : en
Publisher:
Release Date : 2000

Technology Developments For Cryogenic Rocket Engines written by H. Immich and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with categories.

Modern Engineering For Design Of Liquid Propellant Rocket Engines

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Author : Dieter K. Huzel
language : en
Publisher: AIAA
Release Date : 1992

Modern Engineering For Design Of Liquid Propellant Rocket Engines written by Dieter K. Huzel and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Liquid propellant rocket engines categories.

The Stability Of Operation Of A Liquid Fuel Rocket Engine

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Author :
language : en
Publisher:
Release Date : 1961

The Stability Of Operation Of A Liquid Fuel Rocket Engine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.

Advanced Cryogenic Rocket Engine Program Aerospike Nozzle Concept

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Author :
language : en
Publisher:
Release Date : 1968

Advanced Cryogenic Rocket Engine Program Aerospike Nozzle Concept written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.

Technical results obtained at the completion of the contract effort are described for the Advanced Cryogenic Rocket Engine Program, Aerospike. This program includes analysis and preliminary design of an advanced rocket engine using an aerospike nozzle and experimental evaluation of critical technology related to the aerospike concept. Component and system features, physical arrangements, design parameters and details, operational characteristics, and performance have been established for an optimum demonstrator engine. Studies were made of application of a flight engine to certain vehicles. Experimental injector performance investigations and experimental cooling investigations on segment chambers were conducted, producing the target combustion performance. Various materials were studied for long life of thrust chamber cooling passages and the target life was demonstrated. Full-scale, cooled thrust chambers were fabricated and tested for overall combustor and nozzle performance demonstrations. Injector failure limited these tests; however, nozzle and combustor performance were as predicted when not influenced by excess leakage. Structural and cooling evaluations were conducted on a segment embodying essential elements of the Demonstrator chamber design. (Author).

Advanced Cryogenic Solid Hybrid Rocket Engine Developments Concept And Test Results

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Author :
language : en
Publisher:
Release Date : 1998

Advanced Cryogenic Solid Hybrid Rocket Engine Developments Concept And Test Results written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.

ORBITEC has conducted considerable R & D under various USAF and NASA contracts and company sponsored efforts to develop a new class of rocket propulsion devices, cryogenic solid rocket engines The basic concept of these engines is to freeze a propellant which is normally a gas at room temperature into a solid propellant grain. This solid grain is then combusted with a second propellant These rocket engines promise a number of advantages over conventional liquid rocket engines, including increased simplicity, safety, propellant density, and potentially performance with the addition of High-Energy Density Matter (HEDM's). ORBITEC has tested cryogenic solid hybrid rocket engines including the following propellant combinations: (1) solid oxygen/gaseous hydrogen; (2) solid hydrogen/gaseous oxygen; (3) solid methane/gaseous oxygen; and (4) solid methane-aluminum/gaseous oxygen. The primary focus of this paper is on solid oxygen/gaseous hydrogen. Work achieved to date includes: (1) a total of over 50 solid oxygen test firings; (2) establishment of regression rate data for the different propellant combinations, where the rates can be a factor of 20 to 40 times higher than conventional HTPB-based hybrids; (3) achievement of burn durations from 1 to 30 seconds; and (4) engine chamber pressures as high as 250 psi The potential applications include. research devices to test high-energy density matter (HEDM); hybrid rocket launch vehicle upper stages; or orbit transfer vehicles. During a current sponsored USAF Research Laboratory (RL, Edwards Air Force Base, CA) project, ORBITEC is to design, develop and test a larger, SOX/LH2 flight-type engine that will have throttling and O/F ratio control.

Orbit Transfer Rocket Engine Technology Program Phase 2 Advanced Engine Study

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Author :
language : en
Publisher:
Release Date : 1987

Orbit Transfer Rocket Engine Technology Program Phase 2 Advanced Engine Study written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with categories.