Add to ORKGFlight qualifications for parachutes were tested on full-scale simulated Viking spacecraft at entry ...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed...
Wind tunnel tests to determine aerodynamic characteristics of Viking spacecraft entry and lander con...
Comparisons are made between the LAURA Navier-Stokes code and Viking Lander Capsule hypersonic aerod...
Results of an investigation to determine the full scale drag coefficient in the high speed, low dens...
An investigation was conducted to obtain flow properties in the wake of the Viking '75 entry vehicle...
An investigation was conducted to obtain flow properties in the wake of a preliminary configuration ...
The flow properties in the wake of 120 degree and 140 degree included angle cones and a model of the...
Tests of the Viking 16.15-meter nominal-diameter disk-gap-band parachute were conducted at Mach numb...
Aerodynamic characteristics of modified conical lifting reentry vehicle at hypersonic speed
Full-scale wind tunnel determination of effect of corrugated canister surface on static aerodynamic ...
A wind tunnel study to determine the supersonic aerodynamic characteristics of a 0.01925-scale model...
Six experimental investigations conducted in the transonic dynamics tunnel, which supported elements...
Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteri...
Flight qualifications for parachutes were tested on full-scale simulated Viking spacecraft at entry ...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed...
Wind tunnel tests to determine aerodynamic characteristics of Viking spacecraft entry and lander con...
Comparisons are made between the LAURA Navier-Stokes code and Viking Lander Capsule hypersonic aerod...
Results of an investigation to determine the full scale drag coefficient in the high speed, low dens...
An investigation was conducted to obtain flow properties in the wake of the Viking '75 entry vehicle...
An investigation was conducted to obtain flow properties in the wake of a preliminary configuration ...
The flow properties in the wake of 120 degree and 140 degree included angle cones and a model of the...
Tests of the Viking 16.15-meter nominal-diameter disk-gap-band parachute were conducted at Mach numb...
Aerodynamic characteristics of modified conical lifting reentry vehicle at hypersonic speed
Full-scale wind tunnel determination of effect of corrugated canister surface on static aerodynamic ...
A wind tunnel study to determine the supersonic aerodynamic characteristics of a 0.01925-scale model...
Six experimental investigations conducted in the transonic dynamics tunnel, which supported elements...
Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteri...
Flight qualifications for parachutes were tested on full-scale simulated Viking spacecraft at entry ...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed...