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2.8% Ares 1 Acoustic Reentry Wind Tunnel Model
2.8% Ares 1 Acoustic Reentry Wind Tunnel Model

Test to determine fluctuating pressure environments from a 2.8% scale Ares I first stage configuration to verify and update reentry…

2.8% Ares I Acoustic Reentry Wind Tunnel Model
2.8% Ares I Acoustic Reentry Wind Tunnel Model

Test to determine fluctuating pressure environments from a 2.8% scale Ares I first stage configuration to verify and update reentry…

Facility Aerodynamics Validations and Operations Research Model
Facility Aerodynamics Validations and Operations Research Model

Cooperative wind tunnel tests to provide engineering insight into facility processes, data reduction, flow quality and a comparative data assessment.

Facility Aerodynamics Validations and Operations Research Model Test Crew
Facility Aerodynamics Validations and Operations Research Model Test Crew

Cooperative wind tunnel tests to provide engineering insight into facility processes, data reduction, flow quality and a comparative data assessment.

6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module
6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module

Test to obtain acoustic data on jet interactions of plume simulations with separation aerodynamic effects for selected specific conditions.

6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module
6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module

Test to obtain acoustic data on jet interactions of plume simulations with separation aerodynamic effects for selected specific conditions.

Ultra High Bypass (UHB) Nacelle Semi Span
Ultra High Bypass (UHB) Nacelle Semi Span

Force, moment, and pressure data measurements of the aerodynamic effects on the inboard underside of the wing near the nacelle…

3% Space Shuttle Aero Acoustics Wind Tunnel Model
3% Space Shuttle Aero Acoustics Wind Tunnel Model

3% space shuttle launch configuration; super light weight (SLWT) external tank with protuberances, orbiter, and RSRB's.

3% Space Shuttle Aero Acoustics Wind Tunnel Model
3% Space Shuttle Aero Acoustics Wind Tunnel Model

3% space shuttle launch configuration; super light weight (SLWT) external tank with protuberances, orbiter, and RSRB's.

5% Scale Model of the Crew Exploration Vehicle (CEV) Alternate Launch Abort System (ALAS)
5% Scale Model of the Crew Exploration Vehicle (CEV) Alternate Launch Abort System (ALAS)

To test force, moment, and pressure data measurements of the jet interference effects on the crew exploration vehicle (CEV) alternate…