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Investigation Of The Static Stability Characteristics Of A Reentry Spacecraft Model In Free Flight For Mach Numbers From 262 To 111 Launched At An Angle Of Attack Of 180
Download Investigation Of The Static Stability Characteristics Of A Reentry Spacecraft Model In Free Flight For Mach Numbers From 262 To 111 Launched At An Angle Of Attack Of 180 full books in PDF, epub, and Kindle. Read online Investigation Of The Static Stability Characteristics Of A Reentry Spacecraft Model In Free Flight For Mach Numbers From 262 To 111 Launched At An Angle Of Attack Of 180 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180° by : J. W. Usry
Download or read book Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180° written by J. W. Usry and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180 Deg by :
Download or read book Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180 Deg written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurments [i.e. Measurements] of Static and Dynamic Stability of Models of the Project Mercury Re-entry Capsule at Mach Numbers 3 and 9.5 by : Simon C. Sommer
Download or read book Free-flight Measurments [i.e. Measurements] of Static and Dynamic Stability of Models of the Project Mercury Re-entry Capsule at Mach Numbers 3 and 9.5 written by Simon C. Sommer and published by . This book was released on 1960 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 by : Dennis E. Fuller
Download or read book Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 written by Dennis E. Fuller and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Longitudinal Stability Characteristics of a 0.067-Scale Model of a Four-Stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65 by : Lloyd S. Jernell
Download or read book Investigation of the Static Longitudinal Stability Characteristics of a 0.067-Scale Model of a Four-Stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65 written by Lloyd S. Jernell and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63 by :
Download or read book Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63 written by and published by . This book was released on 1962 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Stability and Control Characteristics at Mach Numbers of 2.86 and 6.02 and Angles of Attack Up to 95 Deg of a Lenticular-shaped Reentry Vehicle by :
Download or read book Static Longitudinal Stability and Control Characteristics at Mach Numbers of 2.86 and 6.02 and Angles of Attack Up to 95 Deg of a Lenticular-shaped Reentry Vehicle written by and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Stability and Control Characteristics At A Mach Number of 1.99 of a Lenticular-Shaped Reentry Vehicle by :
Download or read book Static Longitudinal Stability and Control Characteristics At A Mach Number of 1.99 of a Lenticular-Shaped Reentry Vehicle written by and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Ablation Effects on Hypersonic Dynamic Stability of a 10 Cone by : Dave R. Moore
Download or read book Investigation of Ablation Effects on Hypersonic Dynamic Stability of a 10 Cone written by Dave R. Moore and published by . This book was released on 1967 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental program has been conducted in the LTV Hypervelocity Wind Tunnel at M = 17 to investigate the effects of ablation product characteristics and thermal lags on re-entry vehicle dynamic stability. The free oscillation method of dynamic stability measurement was used and the ablation processes were simulated by the controlled mass injection through four sections of the porous model skin. The flow rates through the top and bottom quadrants were oscillated at the same frequency and at an amplitude proportional to the model motion. The thermal lag effect was investigated with nitrogen injection into nitrogen tunnel flow at several different mass flow rates and phase angles between the oscillating mass flow and the body motion. The ablation product study was conducted by injecting gases other than nitrogen with specific heat ratio and molecular weight being the test parameters in addition to mass flow rate. The results obtained from these tests indicate significant effect on dynamic stability with both injection phase angle and some characteristics of the injected gas. The effects of model frequency, Reynolds number and mass injection distribution were also investigated and some static pressure measurements were made near the aft of the model. Appendices to the report contain tabulations of the pertinent data and discussions of supporting analytical studies and data analysis.
Book Synopsis Static Stability and Control Characteristics at Low-subsonic Speeds of a Lenticular Reentry Configuration by : George M. Ware
Download or read book Static Stability and Control Characteristics at Low-subsonic Speeds of a Lenticular Reentry Configuration written by George M. Ware and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Static Stability Characteristics of Several Preliminary Models of the X-15 Research Airplane at Mach Numbers of 2.98 and 4.01 by : Robert W. Dunning
Download or read book The Static Stability Characteristics of Several Preliminary Models of the X-15 Research Airplane at Mach Numbers of 2.98 and 4.01 written by Robert W. Dunning and published by . This book was released on 1959 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Longitudinal Stability Characteristics of a Model of an Intermediate-range Ballistic Missile at Mach Numbers Between 1.57 and 4.65 by : Robert M. Lust
Download or read book Investigation of the Static Longitudinal Stability Characteristics of a Model of an Intermediate-range Ballistic Missile at Mach Numbers Between 1.57 and 4.65 written by Robert M. Lust and published by . This book was released on 1960 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wingless Flight written by R. Dale Reed and published by University Press of Kentucky. This book was released on 2014-07-15 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt: Most lifting bodies, or "flying bathtubs" as they were called, were so ugly only an engineer could love them, and yet, what an elegant way to keep wings from burning off in supersonic flight between earth and orbit. Working in their spare time (because they couldn't initially get official permission), Dale Reed and his team of engineers demonstrated the potential of the design that led to the Space Shuttle. Wingless Flight takes us behind the scenes with just the right blend of technical information and fascinating detail (the crash of M2-F2 found new life as the opening credit for TV's "The Six Million Dollar Man"). The flying bathtub, itself, is finding new life as the proposed escape-pod for the Space Station.
Book Synopsis Technical Report - Jet Propulsion Laboratory, California Institute of Technology by : Jet Propulsion Laboratory (U.S.)
Download or read book Technical Report - Jet Propulsion Laboratory, California Institute of Technology written by Jet Propulsion Laboratory (U.S.) and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-subsonic Aerodynamic Characteristics of a Model of a Modified Lenticular Reentry Configuration by : George M. Ware
Download or read book Investigation of the Low-subsonic Aerodynamic Characteristics of a Model of a Modified Lenticular Reentry Configuration written by George M. Ware and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Several Nose and Vertical-fin Modifications on the Low-angle-of-attack Static Stability of a Winged Reentry Vehicle at Mach Numbers of 9.6 in Air and 17.8 in Helium by :
Download or read book Effects of Several Nose and Vertical-fin Modifications on the Low-angle-of-attack Static Stability of a Winged Reentry Vehicle at Mach Numbers of 9.6 in Air and 17.8 in Helium written by and published by . This book was released on 1961 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Atmospheric Reentry for the Space Maneuver Vehicle by : Dennis J. McNabb
Download or read book Investigation of Atmospheric Reentry for the Space Maneuver Vehicle written by Dennis J. McNabb and published by . This book was released on 2004-03-01 with total page 95 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study investigated the atmospheric reentry of the Space Maneuver Vehicle from low-earth orbit using an entry guidance concept similar to the Space Shuttle. The Space Maneuver Vehicle was modeled as a point mass with aerodynamic properties as determined using Newtonian impact theory. For the rarefied-flow transition regime bridging formulae are used to capture the effects of both hypersonic continuum flow and free molecular flow. Constraints to the reentry are developed and a reentry corridor is defined in the drag- velocity plane. Bank angle modulation is established as the primary means for controlling drag and range. The guidance concept is applied to both a high inclination orbit and a low inclination orbit with cross-range requirement. Monte Carlo error analysis validates the ability of the control algorithm to guide reentry in the presence of initial state errors, as well as atmospheric variations. (7 tables, 54 figures, 18 refs.)
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