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Book Static Longitudinal Stability and Performance of Several Ballistic Spacecraft Configuration in Helium at a Mach Number of 24 5

Download or read book Static Longitudinal Stability and Performance of Several Ballistic Spacecraft Configuration in Helium at a Mach Number of 24 5 written by Patrick J. Johnston and published by . This book was released on 1962 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Stability and Performance of Several Ballistic Spacecraft Configuration in Helium at a Mach Number of 24 5

Download or read book Static Longitudinal Stability and Performance of Several Ballistic Spacecraft Configuration in Helium at a Mach Number of 24 5 written by Patrick J. Johnston and published by . This book was released on 1962 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Stability and Performance of Several Ballistic Spacecraft Configurations in Helium at a Mach Number 24 5

Download or read book Static Longitudinal Stability and Performance of Several Ballistic Spacecraft Configurations in Helium at a Mach Number 24 5 written by Patrick J. Johnston and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Note

Download or read book NASA Technical Note written by and published by . This book was released on 1965 with total page 842 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Reynolds Number Effects on the Induced Pressures of Cylindrical Bodies with Different Nose Shapes and Nose Drag Coefficients in Helium at a Mach Number of 24

Download or read book Reynolds Number Effects on the Induced Pressures of Cylindrical Bodies with Different Nose Shapes and Nose Drag Coefficients in Helium at a Mach Number of 24 written by Richard D. Wagner (Jr.) and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Exact inviscid pressure distributions and shock shapes, obtained by the method of characteristics, are compared with experimental data. The results indicate a strong dependence of induced pressures upon Reynolds number, especially in the region immediately downstream of the nose-cylinder junction. The measured shock shapes revealed no discernible effect of Reynolds number variations.

Book Aerodynamic Characteristics of Several Lifting and Nonlifting Configurations at Hypersonic Speeds in Air and Helium

Download or read book Aerodynamic Characteristics of Several Lifting and Nonlifting Configurations at Hypersonic Speeds in Air and Helium written by James P. Arrington and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Longitudinal Aerodynamic Characteristics of Several Fifth stage Scout Reentry Vehicles from Mach Number 0 60 to 24 4 Including Some Reynolds Number Effects on Stability at Hypersonic Speeds

Download or read book Longitudinal Aerodynamic Characteristics of Several Fifth stage Scout Reentry Vehicles from Mach Number 0 60 to 24 4 Including Some Reynolds Number Effects on Stability at Hypersonic Speeds written by Patrick J. Johnston and published by . This book was released on 1963 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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 Static Stability Investigations of Proposed Project Fire Space vehicle and Reentry package Configurations at Mach Numbers from 1 47 to 4 63

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 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

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 Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three stage Missile Configuration at Mach Numbers from 1 77 to 2 87

Download or read book Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three stage Missile Configuration at Mach Numbers from 1 77 to 2 87 written by Donald T. Gregory and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Stability and Control Characteristics at a Mach Number of 2 01 of a Hypersonic Missile Configuration Having All movable Wing and Tail Surfaces

Download or read book Static Longitudinal Stability and Control Characteristics at a Mach Number of 2 01 of a Hypersonic Missile Configuration Having All movable Wing and Tail Surfaces written by Ross B. Robinson and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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:

Book Static Stability Characteristics of Blunt Low fineness ratio Bodies of Revolution at a Mach Number of 24 5 in Helium

Download or read book Static Stability Characteristics of Blunt Low fineness ratio Bodies of Revolution at a Mach Number of 24 5 in Helium written by Robert D. Witcofski and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: