The Aerosciences Branch (EV33) at the George C. Marshall Space Flight Center (MSFC) has been responsible for a series of wind tunnel tests on the National Aeronautics and Space Administration's (NASA) Space Launch System (SLS) vehicles. The primary purpose of these tests was to obtain aerodynamic data during the ascent phase and establish databases that can be used by the Guidance, Navigation, and Mission Analysis Branch (EV42) for trajectory simulations. The paper describes the test particulars regarding models and measurements and the facilities used, as well as database preparations
Characterization of accurate flight vehicle unsteady aerodynamics is critical for component and seco...
Wind tunnel tests to evaluate the flight characteristics of several expendable second stage/payload ...
NASA-Langley Research Center is conducting system level studies on an-house concept of a small launc...
This paper describes the wind tunnel testing work and data analysis required to characterize the sta...
The Space Launch System Aerodynamics Task Team is responsible for delivering aerodynamic force and m...
Aerodynamic environments are some of the rst engineering data products that are needed to design a s...
The development of the aerodynamic database for the Space Launch System (SLS) booster separation env...
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Resea...
NASA Langley Research Center, in partnership with NASA Marshall Space Flight Center and NASA Ames Re...
A wind-tunnel investigation of a 0.009 scale model of the Space Launch System (SLS) was conducted in...
The objective of this paper is to document the reasoning and trade studies that supported the select...
During the launching vehicles design and their optimization process, the implementing of aerodynamic...
The Space Shuttle aerodynamics and performance communities were challenged to verify the Space Shutt...
A modern launch vehicle is by necessity an extremely integrated design. The accurate characterizatio...
A detailed description of the uncertainty quantification process for the Space Launch System Block 1...
Characterization of accurate flight vehicle unsteady aerodynamics is critical for component and seco...
Wind tunnel tests to evaluate the flight characteristics of several expendable second stage/payload ...
NASA-Langley Research Center is conducting system level studies on an-house concept of a small launc...
This paper describes the wind tunnel testing work and data analysis required to characterize the sta...
The Space Launch System Aerodynamics Task Team is responsible for delivering aerodynamic force and m...
Aerodynamic environments are some of the rst engineering data products that are needed to design a s...
The development of the aerodynamic database for the Space Launch System (SLS) booster separation env...
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Resea...
NASA Langley Research Center, in partnership with NASA Marshall Space Flight Center and NASA Ames Re...
A wind-tunnel investigation of a 0.009 scale model of the Space Launch System (SLS) was conducted in...
The objective of this paper is to document the reasoning and trade studies that supported the select...
During the launching vehicles design and their optimization process, the implementing of aerodynamic...
The Space Shuttle aerodynamics and performance communities were challenged to verify the Space Shutt...
A modern launch vehicle is by necessity an extremely integrated design. The accurate characterizatio...
A detailed description of the uncertainty quantification process for the Space Launch System Block 1...
Characterization of accurate flight vehicle unsteady aerodynamics is critical for component and seco...
Wind tunnel tests to evaluate the flight characteristics of several expendable second stage/payload ...
NASA-Langley Research Center is conducting system level studies on an-house concept of a small launc...