Download or read book Aerodynamic Stability Characteristics of the Apollo Command Module written by William C. Moseley (Jr.) and published by . This book was released on 1968 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

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:

Download or read book Stability Characteristics of the Apollo Command Module written by William C. Moseley and published by . This book was released on 1967 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Technical Note written by and published by . This book was released on 1967 with total page 478 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

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:

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:

Download or read book Entry Flight Aerodynamics from Apollo Mission AS 202 written by E. R. Hillje and published by . This book was released on 1967 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation of the Aerodynamic Pressures on the Apollo Command Module Configuration written by William C. Moseley and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind tunnel study of aerodynamic pressures on Apollo command module configuration.

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:

Download or read book Effects of Two Probe Antennas on Aerodynamic Characteristics of Apollo Spacecraft at Mach 10 03 written by Lawrence E. Putnam and published by . This book was released on 1967 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Longitudinal Aerodynamic Characteristics of a Powered Model of the Apollo Launch escape Vehicle from Mach 0 50 to 1 30 written by and published by . This book was released on 1966 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Landing Characteristics of the Apollo Spacecraft with Deployed heat shield Impact Attenuation Systems written by Sandy M. Stubbs and published by . This book was released on 1966 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was made to determine the landing characteristics of a 1/4-scale dynamic model of the Apollo spacecraft command module using two different active (heat shield deployed prior to landing) landing systems for impact attenuation. One landing system (configuration 1) consisted of six hydraulic struts and eight crushable honeycomb struts. The other landing system (configuration 2), consisting of four hydraulic struts and six strain straps, was lighter. Tests made on water and the hard clay-gravel composite landing surfaces simulated parachute letdown (vertical) velocities of 23 ft/sec (7.0 m/s) (full scale). Landings made on the sand landing surface simulated vertical velocities of 30 ft/sec (9.1 m/s). Horizontal velocities of from 0 to 50 ft/sec (15 m/s) were simulated. Landing attitudes ranged from -30 degrees to 20 degrees , and the roll attitudes were 0 degrees, 90 degrees, and 180 degrees.

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:

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:

Download or read book Effects of Front face Asymmetry on the Aerodynamic Characteristics of the Apollo Capsule written by and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: