Numerical analysis of techniques for separating space shuttles by separation rockets, spring loaded ram, nonignitable gas ejector, or pyrotechnic ra
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...
Photoelastic investigation on scaled models of Algol rocket engine nozzles to determine pressure and...
Pyrotechnic shock analysis and testing methods for Ranger and Mariner spacecraft measurement
Tabulated source data are presented of the results of aerodynamic investigations conducted on the se...
Data figures are presented of the results of aerodynamic investigations conducted on the separation ...
The results of studies and software development activities are summarized. Technical reports and mem...
Proceedings of conference on space shuttle aerothermodynamics with emphasis on operational flight me...
Engineering drawings are presented which represent the culmination of research efforts towards a spa...
The Phase B Extension of the Space Shuttle System Program Definition study was redirected to apply p...
IBM 7090 digital computer program for solving equations of motion for spacecraft separating from fin...
Conference on ground operations, flight operations, and safety for space shuttle program - Vol.
The integrated space shuttle vehicle was tested to determine proximity force and moment data for the...
A study for the selection of a low cost shuttle system for design and development was conducted. The...
The development of space shuttle separation devices is reviewed to illustrate the mechanisms involve...
This is a presentation of view graphs. The design parameters are given for the redesigned solid rock...
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...
Photoelastic investigation on scaled models of Algol rocket engine nozzles to determine pressure and...
Pyrotechnic shock analysis and testing methods for Ranger and Mariner spacecraft measurement
Tabulated source data are presented of the results of aerodynamic investigations conducted on the se...
Data figures are presented of the results of aerodynamic investigations conducted on the separation ...
The results of studies and software development activities are summarized. Technical reports and mem...
Proceedings of conference on space shuttle aerothermodynamics with emphasis on operational flight me...
Engineering drawings are presented which represent the culmination of research efforts towards a spa...
The Phase B Extension of the Space Shuttle System Program Definition study was redirected to apply p...
IBM 7090 digital computer program for solving equations of motion for spacecraft separating from fin...
Conference on ground operations, flight operations, and safety for space shuttle program - Vol.
The integrated space shuttle vehicle was tested to determine proximity force and moment data for the...
A study for the selection of a low cost shuttle system for design and development was conducted. The...
The development of space shuttle separation devices is reviewed to illustrate the mechanisms involve...
This is a presentation of view graphs. The design parameters are given for the redesigned solid rock...
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...
Photoelastic investigation on scaled models of Algol rocket engine nozzles to determine pressure and...
Pyrotechnic shock analysis and testing methods for Ranger and Mariner spacecraft measurement