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Some Dynamic Stability Characteristics Of Models Of Proposed Apollo Configurations At Mach Numbers From 160 To 275
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Book Synopsis Some Dynamic Stability Characteristics of Models of Proposed Apollo Configurations at Mach Numbers from 1.60 to 2.75 by :
Download or read book Some Dynamic Stability Characteristics of Models of Proposed Apollo Configurations at Mach Numbers from 1.60 to 2.75 written by and published by . This book was released on 1964 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Dynamic-stability Characteristics of Models of Proposed Apollo Configurations at Mach Numbers from 0.30 to 1.20 by :
Download or read book Dynamic-stability Characteristics of Models of Proposed Apollo Configurations at Mach Numbers from 0.30 to 1.20 written by and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Dynamic Stability Characteristics in Pitch of Models of Proposed Apollo Configurations at Mach Numbers from 0.30 to 4.63 by :
Download or read book Dynamic Stability Characteristics in Pitch of Models of Proposed Apollo Configurations at Mach Numbers from 0.30 to 4.63 written by and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Measurements of Some Dynamic Stability Characteristics of 0.555 Scale Models of Proposed Apollo Command Module and Launch Escape Configurations at Mach Numbers from 2.40 to 4.65 by :
Download or read book Wind Tunnel Measurements of Some Dynamic Stability Characteristics of 0.555 Scale Models of Proposed Apollo Command Module and Launch Escape Configurations at Mach Numbers from 2.40 to 4.65 written by and published by . This book was released on 1963 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability Characteristics of the Apollo Command Module by : William C. Moseley (Jr.)
Download or read book Stability Characteristics of the Apollo Command Module written by William C. Moseley (Jr.) and published by . This book was released on 1967 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle by : William C. Moseley (Jr.)
Download or read book Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle written by William C. Moseley (Jr.) and published by . This book was released on 1967 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control Characteristics of a 0.030-scale Model of a Little Joe 2-Apollo Space Vehicle at Mach Numbers from 1.57 to 4.65 by :
Download or read book Static Stability and Control Characteristics of a 0.030-scale Model of a Little Joe 2-Apollo Space Vehicle at Mach Numbers from 1.57 to 4.65 written by and published by . This book was released on 1963 with total page 28 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 Forces and Moments on an Apollo Model in Air at Mach Numbers to 35 and Effects of Changing Face and Corner Radii by :
Download or read book Forces and Moments on an Apollo Model in Air at Mach Numbers to 35 and Effects of Changing Face and Corner Radii written by and published by . This book was released on 1965 with total page 68 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 Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Models of Reentry and Atmospheric-abort Configurations of a Proposed Apollo Spacecraft at Mach Numbers from 0.30 to 1.20 by :
Download or read book Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Models of Reentry and Atmospheric-abort Configurations of a Proposed Apollo Spacecraft at Mach Numbers from 0.30 to 1.20 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 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 An Investigation of the Dynamic Stability and Control Characteristics for a Transport Cruising at a Mach Number of 3 by : Lawrence W. Brown
Download or read book An Investigation of the Dynamic Stability and Control Characteristics for a Transport Cruising at a Mach Number of 3 written by Lawrence W. Brown and published by . This book was released on 1964 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of a Modified Model of a Proposed Apollo Atmospheric Abort Configuration at Mach Numbers from 0.30 to 1.20 by : Albin O. Pearson
Download or read book Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of a Modified Model of a Proposed Apollo Atmospheric Abort Configuration at Mach Numbers from 0.30 to 1.20 written by Albin O. Pearson and published by . This book was released on 1962 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of a Model of a Two-stage Version of a Saturn Launch Vehicle with a Proposed Apollo Payload at Mach Numbers from 1.57 to 2.87 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a Model of a Two-stage Version of a Saturn Launch Vehicle with a Proposed Apollo Payload at Mach Numbers from 1.57 to 2.87 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 Aerodynamic Characteristics Determined During Development of the Apollo Launch Escape Vehicle Configuration by : William C. Moseley (Jr.)
Download or read book Aerodynamic Characteristics Determined During Development of the Apollo Launch Escape Vehicle Configuration written by William C. Moseley (Jr.) and published by . This book was released on 1969 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Static and Dynamic Stability Characteristics of Several Saturn Ib and V Upper Stage Configurations by : R. I. Lowndes
Download or read book Transonic Static and Dynamic Stability Characteristics of Several Saturn Ib and V Upper Stage Configurations written by R. I. Lowndes and published by . This book was released on 1966 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Dynamic stability characteristics of six Apollo-Saturn 1B and 5 and one Saturn-Centaur upper stage model configurations and static stability characteristics of two Apollo-Saturn B and 5 upper stage model configurations were obtained from M = 0.50 to 1.40. The primary test objective was to investigate the changes in dynamic stability characteristics as a function of pitch oscillation center. A secondary objective was to compare three different model mounting techniques - sting, transverse rod, and reflection plane. The static testing resulted from a suspected nonlinear phenomenon observed during the dynamic phase of the test. One model configuration which was stable when the pitch oscillation center was ahead of a separation disk exhibited limit cycle oscillations when the pitch oscillation center was located aft of the disk. (Author).
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