Download or read book Liquid Oxygen Cooling of High Pressure LOX hydrocarbon Rocket Thrust Chambers written by and published by . This book was released on 1986 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Liquid Oxygen Cooling of Hydrocarbon Fueled Rocket Thrust Chambers written by Elizabeth S. Armstrong and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High pressure Calorimeter Chamber Tests for Liquid Oxygen kerosene LOX RP 1 Rocket Combustion written by Philip A. Masters and published by . This book was released on 1988 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Cooling Problems at High Chamber Pressures written by and published by . This book was released on 1963 with total page 401 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Analytical and experimental results are presented of an investigation to develop the enineering data and technology required to design cooling systems for liquid propellant rocket engines operating at chamber pressures from 1500 to 500 psia, at thrust levels up to 6 million pounds, and using liquid oxygen/hydrocarbon and liquid oxygen/liquid hydrogen as propellants."--p.iii.
Download or read book Theoretical Performance of Hydrogen oxygen Rocket Thrust Chambers written by Gilbert K. Sievers and published by . This book was released on 1961 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Cooling Problems at High Chamber Pressures written by Research and Advanced Projects Departments and published by . This book was released on 1965 with total page 423 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Analytical and experimental results are presented of a continuation of the investigation to develop the enineering data and technology required to design cooling systems for liquid propellant rocket engines operating at chamber pressures from 1500 to 5000 psia, at thrust levels up to 6 million pounds, and using liquid oxygen/hydrocarbon and liquid oxygen/liquid hydrogen as propellants."--p.v.
Download or read book High pressure Calorimeter Chamber Tests for Liquid Oxygen kerosene LOX RP 1 Rocket Combustion written by Philip A. Masters and published by . This book was released on 1988 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Dimension Optimizing Design Method For Annular Type Cooling Channel Of Thrust Chamber written by and published by . This book was released on 1995 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: The new-generation liquid oxygen/hydrocarbon propellant liquid fuel rocket engine will use a high-pressure combustion chamber arrangement. In this case, cooling the thrust chamber becomes a key technical problem. The article presents a design scheme for the geometric-dimension optimization of annular-type regenerative cooling channels. The aim of the optimization is minimum pressure losses as coolant passes through the cooling channel. As shown in typical computations and experiments, application of this optimizing design method can reduce 50% of pressure losses. In other words, the optimization design is advantageous in solving the cooling problem in high-pressure thrust chambers. jg.
Download or read book Cooling of Rocket Thrust Chambers with Liquid Oxygen written by Elizabeth S. Armstrong and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Modern Engineering for Design of Liquid Propellant Rocket Engines written by Dieter K. Huzel and published by AIAA. This book was released on 1992 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Liquid Rocket Engine Combustion Instability written by Vigor Young and published by AIAA. This book was released on 1995 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation Since the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.
Download or read book Energy Research Abstracts written by and published by . This book was released on 1989 with total page 760 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transpiration Cooling of Rocket Thrust Chamber with Liquid Oxygen written by Liu Weiqiang and published by . This book was released on 1998 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Fed Thrust Chamber Technology Program written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-14 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is the final report for the Pressure Fed Technology Program. It details the design, fabrication, and testing of subscale hardware which successfully characterized Liquid Oxygen Rocket Propulsion (LOX/RP) combustion for low cost pressure fed design. The innovative modular injector design is described in detail as well as hot-fire test results which showed excellent performance. The program summary identifies critical LOX/RP design issues that have been resolved in this testing, and details the low risk development requirements for low cost engines for future Expandable Launch Vehicles (ELV). Dunn, Glen M. Unspecified Center LIQUID PROPELLANT ROCKET ENGINES; PERFORMANCE TESTS; PRESSURE EFFECTS; PROPULSION SYSTEM CONFIGURATIONS; TECHNOLOGY ASSESSMENT; THRUST CHAMBERS; FABRICATION; INJECTORS; LAUNCH VEHICLES; LIQUID OXYGEN; LOW COST...
Download or read book Cryogenic Information Report written by and published by . This book was released on 1989 with total page 354 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1988 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
