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EBookClubs

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Book Optimization of an Air Augmented Rocket System

Download or read book Optimization of an Air Augmented Rocket System written by Liborio Jose Faria and published by . This book was released on 1971 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Air Augmented Rocket Propulsion Concepts

Download or read book Air Augmented Rocket Propulsion Concepts written by R. W. Foster and published by . This book was released on 1988 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Operationally Efficient Propulsion System Study  Oepss  Data Book  Volume 10  Air Augmented Rocket Afterburning

Download or read book Operationally Efficient Propulsion System Study Oepss Data Book Volume 10 Air Augmented Rocket Afterburning written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-09 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was directed towards assessing viability and effectiveness of an air augmented ejector/rocket. Successful thrust augmentation could potentially reduce a multi-stage vehicle to a single stage-to-orbit vehicle (SSTO) and, thereby, eliminate the associated ground support facility infrastructure and ground processing required by the eliminated stage. The results of this preliminary study indicate that an air augmented ejector/rocket propulsion system is viable. However, uncertainties resulting from simplified approach and assumptions must be resolved by further investigations. Farhangi, Shahram and Trent, Donnie (Editor) Kennedy Space Center NAS10-11568...

Book Turbo air Augmented Rocket

Download or read book Turbo air Augmented Rocket written by A. R. Ganji and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Liquid Air Augmented Rocket Engine for a Small Reusable SSTO Launcher

Download or read book Liquid Air Augmented Rocket Engine for a Small Reusable SSTO Launcher written by V. Balepin and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Air Augmented Rocket Propellant Screening Facility

Download or read book Air Augmented Rocket Propellant Screening Facility written by Charles H. Hitchcock and published by . This book was released on 1971 with total page 185 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report summarizes the results of an Air Force Rocket Propulsion Laboratory engineering development effort to design, fabricate and activate a laboratory-scale, direct-connect test facility. The facility, composed of a clean air supply system, a primary solid rocket combustor and a ramburner, is designed to support air-augmented rocket propellant development efforts. The versatile facility design allows variation in hardware configuration and propellant flow parameters to simulate a broad range of flight conditions, i.e., Mach No. 2 to 3.5 and altitudes from sea level to 50,000 feet. The air delivery system is designed for maximum conditions of 7 lb/sec, 1000F and 250 psia. The annular inlet manifold is adaptable to either a 2-inch-diameter, center-perforated or 6-inch-diameter, end burning primary combustor. A variable-length, 5-inch-diameter ramburner is used. The combustion processes occurring in the primary and secondary chambers are monitored by means of wall pressure and temperature measurements, thrust measurement, residue sampling and optical techniques. Facility performance capabilities, system calibration and preliminary evaluation of baseline direct-connect testing are presented. (Author).

Book A Review of Air augmented Rocket Propulsion for Guided Weapons

Download or read book A Review of Air augmented Rocket Propulsion for Guided Weapons written by A. W. Mowat and published by . This book was released on 1973 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Simple Calculation of the Thrust of an Air augmented Rocket

Download or read book A Simple Calculation of the Thrust of an Air augmented Rocket written by K. N. C. Bray and published by . This book was released on 1974 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 912 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Liquid Air Augmented Rocket for Future Launches

Download or read book Liquid Air Augmented Rocket for Future Launches written by Laurence Couteaux and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs

Download or read book A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs written by National Research Council and published by National Academies Press. This book was released on 2007-01-14 with total page 288 pages. Available in PDF, EPUB and Kindle. Book excerpt: Rocket and air-breathing propulsion systems are the foundation on which planning for future aerospace systems rests. A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs assesses the existing technical base in these areas and examines the future Air Force capabilities the base will be expected to support. This report also defines gaps and recommends where future warfighter capabilities not yet fully defined could be met by current science and technology development plans.

Book Air Augmented Rocket Fixed Fuel Flow Combustion Characterization Program

Download or read book Air Augmented Rocket Fixed Fuel Flow Combustion Characterization Program written by Jerry L. Fields and published by . This book was released on 1973 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: This program demonstrated that reliable, consistent combustion efficiency data could be obtained independently at different facilities. The detailed combustion efficiency performance of two Boron loaded fuel rich propellants was mapped over an air-to-fuel ratio range from 10 to 40 and a ramburner air-only pressure range from 13 to 40 psia. Two highly loaded Boron propellants were used. Testing was conducted at three facilities. Six inch subscale hardware was utilized and a coaxial mixing configuration chosen. Data analysis procedures were refined and error sources (particularly fuel flow rate uncertainties) minimized. The averaged combustion efficiency data from all three facilities fell within the computed error bands, + or - 5.5 percent. Significant A/F dependence was found for combustion efficiency for the two propellants. The effect of fuel generator pressure on combustion efficiency was briefly investigated and found to be negligible. Finally, a propellant comparison was made and ARC 256A had generally better combustion efficiency performance and a higher theoretical heating value, leading to its selection as the superior propellant. (Author).