Add to ORKGAn experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
A fully operational space shuttle is discussed which will offer science the opportunity to explore n...
The results of a study are presented in which a computerized optimal control techique was applied to...
The prediction of flight loads and their potential reduction, using various control system logics fo...
A space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce ...
The basic guidance and control concepts that lead to structural control interaction and structural d...
The atmospheric ascent flight phase of the mated composite booster and orbiter is discussed. The com...
The steering system of the space shuttle vehicle is presented for the several hundred miles of fligh...
Data measurement and interpretation techniques were defined for application to the first few space s...
From the beginning of the Shuttle Program to its end, integrated loads and dynamics analyses and tes...
Static longitudinal, directional, and lateral characteristics and control surface effectiveness of s...
Designs and data for selecting aerodynamic surface control and thrust vector control servoactuato
A study of one shuttle orbiter approach and landing conditions are summarized. Causes of observed PI...
The derivations of mathematical models in Vol. 1 are presented along with descriptions of all periph...
A study was conducted in a trisonic wind tunnel to determine the load distribution over the external...
An experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
A fully operational space shuttle is discussed which will offer science the opportunity to explore n...
The results of a study are presented in which a computerized optimal control techique was applied to...
The prediction of flight loads and their potential reduction, using various control system logics fo...
A space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce ...
The basic guidance and control concepts that lead to structural control interaction and structural d...
The atmospheric ascent flight phase of the mated composite booster and orbiter is discussed. The com...
The steering system of the space shuttle vehicle is presented for the several hundred miles of fligh...
Data measurement and interpretation techniques were defined for application to the first few space s...
From the beginning of the Shuttle Program to its end, integrated loads and dynamics analyses and tes...
Static longitudinal, directional, and lateral characteristics and control surface effectiveness of s...
Designs and data for selecting aerodynamic surface control and thrust vector control servoactuato
A study of one shuttle orbiter approach and landing conditions are summarized. Causes of observed PI...
The derivations of mathematical models in Vol. 1 are presented along with descriptions of all periph...
A study was conducted in a trisonic wind tunnel to determine the load distribution over the external...
An experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
A fully operational space shuttle is discussed which will offer science the opportunity to explore n...
The results of a study are presented in which a computerized optimal control techique was applied to...