Investigation of a Large Winged First Stage of a VTO Reusable Orbital Launch Vehicle from Mach 2.3 to 6.0

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Investigation of a Large Winged First Stage of a VTO Reusable Orbital Launch Vehicle from Mach 2.3 to 6.0 by :

Download or read book Investigation of a Large Winged First Stage of a VTO Reusable Orbital Launch Vehicle from Mach 2.3 to 6.0 written by and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Summary Aerodynamic Characteristics of a VTO Reusable Launch Vehicle from Mach 0.2 to 6.0

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Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Summary Aerodynamic Characteristics of a VTO Reusable Launch Vehicle from Mach 0.2 to 6.0 by :

Download or read book Summary Aerodynamic Characteristics of a VTO Reusable Launch Vehicle from Mach 0.2 to 6.0 written by and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Investigation of a Large Winged Vertical Take Off Reusable Orbital Launch Vehicle at Mach 0.4 to 2.1

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Publisher :
ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Investigation of a Large Winged Vertical Take Off Reusable Orbital Launch Vehicle at Mach 0.4 to 2.1 by :

Download or read book Aerodynamic Investigation of a Large Winged Vertical Take Off Reusable Orbital Launch Vehicle at Mach 0.4 to 2.1 written by and published by . This book was released on 1964 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Complete VTO Launch Vehicle and Reusable Flyback Configuration from Mach 3.0 to 6.0

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Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Characteristics of a Complete VTO Launch Vehicle and Reusable Flyback Configuration from Mach 3.0 to 6.0 by :

Download or read book Aerodynamic Characteristics of a Complete VTO Launch Vehicle and Reusable Flyback Configuration from Mach 3.0 to 6.0 written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Exploratory Study of Parallel-stage Separation of Reusable Launch Vehicles

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Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis An Exploratory Study of Parallel-stage Separation of Reusable Launch Vehicles by : John P. Decker

Download or read book An Exploratory Study of Parallel-stage Separation of Reusable Launch Vehicles written by John P. Decker and published by . This book was released on 1968 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Reusable Launch Vehicle

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Publisher : National Academies Press
ISBN 13 : 0309175860
Total Pages : 98 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Reusable Launch Vehicle by : National Research Council

Download or read book Reusable Launch Vehicle written by National Research Council and published by National Academies Press. This book was released on 1996-01-08 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: The key to opening the use of space to private enterprise and to broader public uses lies in reducing the cost of the transportation to space. More routine, affordable access to space will entail aircraft-like quick turnaround and reliable operations. Currently, the space Shuttle is the only reusable launch vehicle, and even parts of it are expendable while other parts require frequent and extensive refurbishment. NASA's highest priority new activity, the Reusable Launch Vehicle program, is directed toward developing technologies to enable a new generation of space launchers, perhaps but not necessarily with single stage to orbit capability. This book assesses whether the technology development, test and analysis programs in propulsion and materials-related technologies are properly constituted to provide the information required to support a December 1996 decision to build the X-33, a technology demonstrator vehicle; and suggest, as appropriate, necessary changes in these programs to ensure that they will support vehicle feasibility goals.

Transonic Characteristics of Both Launch and Flyback Configurations of a VTO Reusable Launch Vehicle

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Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Transonic Characteristics of Both Launch and Flyback Configurations of a VTO Reusable Launch Vehicle by :

Download or read book Transonic Characteristics of Both Launch and Flyback Configurations of a VTO Reusable Launch Vehicle written by and published by . This book was released on 1965 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs

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Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs by : Peter H. Urschel

Download or read book Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs written by Peter H. Urschel and published by . This book was released on 2003 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Separation Characteristics of Conceptual Parallel-staged Reusable Launch Vehicle at Mach 3 to Mach 6

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Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Separation Characteristics of Conceptual Parallel-staged Reusable Launch Vehicle at Mach 3 to Mach 6 by :

Download or read book Aerodynamic Separation Characteristics of Conceptual Parallel-staged Reusable Launch Vehicle at Mach 3 to Mach 6 written by and published by . This book was released on 1965 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analysis of the Staging Maneuver and Booster Glideback Guidance for a Two-stage, Winged, Fully Reusable Launch Vehicle

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Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Analysis of the Staging Maneuver and Booster Glideback Guidance for a Two-stage, Winged, Fully Reusable Launch Vehicle by : J. Christopher Naftel

Download or read book Analysis of the Staging Maneuver and Booster Glideback Guidance for a Two-stage, Winged, Fully Reusable Launch Vehicle written by J. Christopher Naftel and published by . This book was released on 1993 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle

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Publisher :
ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle by : Anhtuan D. Ngo

Download or read book Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle written by Anhtuan D. Ngo and published by . This book was released on 2003 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this paper, we will examine a configuration for a reusable military launch vehicle (RMLS) concept. This configuration allows for the vehicle to land in an inverted attitude. Such inverted landing improves the turnaround time of the vehicle by reducing the maintenance requirements of the vehicle's thermal protection system. An analysis is performed to examine the impacts by the configuration on stability, control, and footprint for an RMLS configuration.

Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65

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Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 by : Dennis E. Fuller

Download or read book Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 written by Dennis E. Fuller and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781720610045
Total Pages : 40 pages
Book Rating : 4.6/5 (1 download)

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Book Synopsis Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs by : National Aeronautics and Space Administration (NASA)

Download or read book Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Defense Advanced Research Projects Agency has proposed a two-stage system to deliver a small payload to orbit. The proposal calls for an airplane to perform an exo-atmospheric zoom climb maneuver, from which a second-stage rocket is launched carrying the payload into orbit. The NASA Dryden Flight Research Center has conducted an in-house generic simulation study to determine how accurately a human-piloted airplane can deliver a second-stage rocket to a desired exo-atmospheric launch condition. A high-performance, fighter-type, fixed-base, real-time, pilot-in-the-loop airplane simulation has been modified to perform exo-atmospheric zoom climb maneuvers. Four research pilots tracked a reference trajectory in the presence of winds, initial offsets, and degraded engine thrust to a second-stage launch condition. These launch conditions have been compared to the reference launch condition to characterize the expected deviation. At each launch condition, a speed change was applied to the second-stage rocket to insert the payload onto a transfer orbit to the desired operational orbit. The most sensitive of the test cases was the degraded thrust case, yielding second-stage launch energies that were too low to achieve the radius of the desired operational orbit. The handling qualities of the airplane, as a first-stage vehicle, have also been investigated.Urschel, Peter H. and Cox, Timothy H.Armstrong Flight Research CenterAEROMANEUVERING; CLIMBING FLIGHT; REUSABLE LAUNCH VEHICLES; TRANSFER ORBITS; PAYLOAD TRANSFER; SIMULATION; TRAJECTORIES; CONTROLLABILITY

A Shadowgraph Study of the National Launch System's 1 1/2 Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration

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Publisher :
ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis A Shadowgraph Study of the National Launch System's 1 1/2 Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration by : Darlene C. Pokora

Download or read book A Shadowgraph Study of the National Launch System's 1 1/2 Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration written by Darlene C. Pokora and published by . This book was released on 1994 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Concepts of Operations for a Reusable Launch Vehicle

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 ( download)

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Book Synopsis Concepts of Operations for a Reusable Launch Vehicle by : Michael A. Rampino

Download or read book Concepts of Operations for a Reusable Launch Vehicle written by Michael A. Rampino and published by . This book was released on 1997 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The United States is embarked on a journey toward maturity as a spacefaring nation. One key step along the way is development of a reusable launch vehicle (RLV). The most recent National Space Transportation Policy (August 1994) assigned improvement and evolution of current expendable launch vehicles to the Department of Defense while National Aeronautical Space Administration (NASA) is responsible for working with industry on demonstrating RLV technology. The purpose of this study is to help ensure the US military, especially the USAF, is prepared to take advantage of RLVs should the NASA-led effort to develop an RLV demonstrator prove successful. The focus of this study is an explanation of how the US military could use RLVs, by describing and analyzing two concepts of operations. Four major conclusions resulted from the analysis. First, RLVs have military potential. They can perform a variety of missions including responsive spacelift, reconnaissance, and strike. However, the economic feasibility of using RLVs for earth-to-earth transportation is questionable. Second, design choices for an operational RLV will have effects on risk, cost, capability, and operations efficiency. Trade-offs will have to be made between NASA, commercial, and military requirements if all three parties are to use the same fleet of RLVs. Third, increased investment in propulsion technology development is warranted to ensure success. Fourth, the top priority for the RLV program, even from the military's perspective, should remain cheap and responsive access to space. The research led to three recommendations. First, the US military should become a more active participant in the RLV program to ensure its requirements are defined and incorporated. Second, America should not pursue development of operational RLVs before the technology is ready.

Reusable Launch Vehicles and Space Operations

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Publisher :
ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.3/5 (121 download)

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Book Synopsis Reusable Launch Vehicles and Space Operations by : John E. Ward

Download or read book Reusable Launch Vehicles and Space Operations written by John E. Ward and published by . This book was released on 2000 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Lateral Aerodynamic Characteristics of a Conceptual Horizontal-take-off Reusable Launch Vehicle from Mach 3 to 6

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Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Lateral Aerodynamic Characteristics of a Conceptual Horizontal-take-off Reusable Launch Vehicle from Mach 3 to 6 by :

Download or read book Lateral Aerodynamic Characteristics of a Conceptual Horizontal-take-off Reusable Launch Vehicle from Mach 3 to 6 written by and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: