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Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of Several Simulated Air-launched Ballistic Missiles Having Various Types of Control Surfaces

Ross B. Robinson

Published: 1961

Total Pages: 46

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

Ross B. Robinson

Published: 1961

Total Pages: 32

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

Published: 1961

Total Pages: 32

Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1

Martin T. Moul

Published: 1952

Total Pages: 42

Longitudinal Stability and Control Characteristics of Missile Configurations Having Several Highly Swept Cruciform Fins and Number of Trailing Edge and Fin Tip Controls at Mach Nubmers from 2.21 to 6.01

Published: 1961

Total Pages: 130

Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing-edge Flaps and One Having a Flared Afterbody and All-movable Cont

Published: 1959

Total Pages: 36

Longitudinal Stability and Control Characteristics of Missile Configurations Having Several Highly Swept Cruciform Fins and a Number of Trailing Edge and Fin Tip Controls at Mach Numbers from 2.21 to 6.01

George C. Jr Ashby

Published: 1961

Total Pages: 124

Longitudinal Stability and Control Characteristics of an Air-to-air Missile Configuration at Mach Numbers of 2.30 and 4.60 and Angles of Attack from Minus 45 Deg to 90 Deg

Published: 1963

Total Pages: 28

Longitudinal Stability and Control Characteristics of a Generalized Missile Configuration Employing Several Different Bulk Type Control Schemes at a Mach Number of 6.01

Published: 1963

Total Pages: 84

Longitudinal Stability and Control Characteristics at Mach Numbers of 1.41 and 2.01 of a 67 Degree Swept-wing Airplane Configuration with Canard Control Surfaces

M. Leroy Spearman

Published: 1958

Total Pages: 36