Add to ORKGA summary of the aerodynamic characteristics of the delta orbiter space shuttle vehicle is presented. Selected guidance and control system parameters, flight path geometry, landing performance obtained with winds and turbulence, and the influence of vehicle L/D on that performance are included
The Space Shuttle descent mission planning, mission design, deorbit targeting, and entry guidance ha...
Low speed wind tunnel test to define space shuttle model cruise and landing aerodynamic characterist...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
The results of a study to analyze, design, and evaluate guidance and control systems are presented ...
Guidance and control design studies that were performed for three specific space shuttle candidate v...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
The unsteady aerodynamics of the proposed delta planform, high cross range, shuttle orbiters, are in...
A study of the display requirements for final approach management of the space shuttle orbiter vehic...
Trisonic wind tunnel static stability tests on straight wing and delta wing space shuttle model
Unpowered automatic approaches and landings were conducted to study navigation, guidance, and contro...
This test program was the first wind tunnel investigation of a double delta wing space shuttle orbit...
Longitudinal, lateral, and directional static stability and control characteristics of delta wing sp...
Aerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from...
Unpowered automatic approaches and landings with a CV990 aircraft were conducted to study navigation...
The longitudinal, lateral, and directional aerodynamic characteristics of two space shuttle concepts...
The Space Shuttle descent mission planning, mission design, deorbit targeting, and entry guidance ha...
Low speed wind tunnel test to define space shuttle model cruise and landing aerodynamic characterist...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
The results of a study to analyze, design, and evaluate guidance and control systems are presented ...
Guidance and control design studies that were performed for three specific space shuttle candidate v...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
The unsteady aerodynamics of the proposed delta planform, high cross range, shuttle orbiters, are in...
A study of the display requirements for final approach management of the space shuttle orbiter vehic...
Trisonic wind tunnel static stability tests on straight wing and delta wing space shuttle model
Unpowered automatic approaches and landings were conducted to study navigation, guidance, and contro...
This test program was the first wind tunnel investigation of a double delta wing space shuttle orbit...
Longitudinal, lateral, and directional static stability and control characteristics of delta wing sp...
Aerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from...
Unpowered automatic approaches and landings with a CV990 aircraft were conducted to study navigation...
The longitudinal, lateral, and directional aerodynamic characteristics of two space shuttle concepts...
The Space Shuttle descent mission planning, mission design, deorbit targeting, and entry guidance ha...
Low speed wind tunnel test to define space shuttle model cruise and landing aerodynamic characterist...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...