Add to ORKGStatic and dynamic characteristics of wind tunnel model of parallel staged reusable launch vehicle during stage separatio
This study is the first to report the tests of a parallel-staged TSTO model with dynamic longitudina...
This paper presents details of Computational Fluid Dynamic (CFD) simulations of the Space Launch Sys...
A numerical investigation is conducted around a multistage launch vehicle to examine the influence o...
The separation concept for stage separation of parallel staged space shuttle vehicles is discussed. ...
This paper presents results from an experimental study of stage separation focusing on shock-shear i...
A sensitivity analysis of the factors which affect a successful abort maneuver following a space shu...
NASA has initiated a comprehensive stage separation tool development activity to address the technol...
The effects of several parameters on the relative motions of a space shuttle orbiter design and its ...
An experimental investigation of plume-induced flow separation on the National Launch System (NLS) 1...
In the past two decades, the renewed interest in sustainable space transportation has driven the dev...
Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
NASA's Hyper-X research program was developed primarily to flight demonstrate a supersonic combustio...
A description and typical results of wind tunnel tests carried out to determine the separation chara...
Stage separation dynamics and system related to staging of Atlas Centaur launch vehicle - full scale...
This study is the first to report the tests of a parallel-staged TSTO model with dynamic longitudina...
This paper presents details of Computational Fluid Dynamic (CFD) simulations of the Space Launch Sys...
A numerical investigation is conducted around a multistage launch vehicle to examine the influence o...
The separation concept for stage separation of parallel staged space shuttle vehicles is discussed. ...
This paper presents results from an experimental study of stage separation focusing on shock-shear i...
A sensitivity analysis of the factors which affect a successful abort maneuver following a space shu...
NASA has initiated a comprehensive stage separation tool development activity to address the technol...
The effects of several parameters on the relative motions of a space shuttle orbiter design and its ...
An experimental investigation of plume-induced flow separation on the National Launch System (NLS) 1...
In the past two decades, the renewed interest in sustainable space transportation has driven the dev...
Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
NASA's Hyper-X research program was developed primarily to flight demonstrate a supersonic combustio...
A description and typical results of wind tunnel tests carried out to determine the separation chara...
Stage separation dynamics and system related to staging of Atlas Centaur launch vehicle - full scale...
This study is the first to report the tests of a parallel-staged TSTO model with dynamic longitudina...
This paper presents details of Computational Fluid Dynamic (CFD) simulations of the Space Launch Sys...
A numerical investigation is conducted around a multistage launch vehicle to examine the influence o...