J. D. Gamble

发表

High supersonic stability and control characteristics of a 0.015-scale (remotely controlled elevon) model 49-0 of the space shuttle orbiter tested in the NASA/LaRC 4-foot UPWT (LEG 2) (LA63B)

J. D. Gamble, 1976 .

The development and application of aerodynamic uncertainties: And flight test verification for the space shuttle orbiter

D. R. Cooke, J. D. Gamble, J. M. Underwood, 1985 .

Transonic stability and control characteristics of a 0.015-scale (remotely controlled elevon) model 44-0 of the space shuttle orbiter tested in the NASA/LaRC 8 foot TPT (LA62). [wind tunnel stability tests in transonic wind tunnels]

M. L. Buhl, J. D. Gamble, H. Parrell, 1975 .

A simplified guidance algorithm for lifting aeroassist orbital transfer vehicles

J. D. Gamble, C. J. Cerimele, C. Cerimele, 1985 .

The aerodynamic challenges of the design and development of the space shuttle orbiter

P. O. Romere, G. M. Ware, J. D. Gamble, 1985 .

The development and application of aerodynamic uncertainties in the design of the entry trajectory and flight control system of the Space Shuttle Orbiter

J. D. Gamble, J. C. Young, J. Gamble, 1982 .

Low supersonic stability and control characteristics of .015-scale (remotely controlled elevon) model 44-0 of space shuttle orbiter tests in NASA/LaRC 4-ft UPWT (leg 1) (LA63A). [wind tunnel stability tests

J. D. Gamble, 1975 .

Atmospheric guidance concepts for an aeroassist flight experiment

J. Higgins, J. D. Gamble, C. J. Cerimele, 1988 .

The application of aerodynamic uncertainties in the design of the entry trajectory and flight control system of the space shuttle orbiter

J. D. Gamble, 1983 .

Scaling of parachute dynamic performance

J. D. Gamble, R. L. Barton, 1967 .