Lockheed Martin Missiles and Fire Control’s High Speed Wind Tunnel (HSWT) is a testing facility that characterizes the behaviors of aerospace products. It is a 4x4 foot tri-sonic blow down wind tunnel with a Mach number range of 0.3 to 5.0.  The HSWT has completed over 1650 tests for customers in the aviation, defense and space industries since opening in 1958.  Located in Dallas, Texas, the HSWT administers a wide variety of critical testing to advance new aerospace developments, including:

• Aerodynamic force and moment testing
• Jet interaction testing of maneuvering thrusters
• Flutter analysis including digital high speed video
• Store separation testing to include free separation and captive trajectory
• Pressure measurements (up to 240 locations)
• Surface flow visualization
• Inlet performance evaluation
• Jet engine base-flow simulation using high pressure gas
• Propulsion (wind tunnel and bench testing)
• Spin/roll damping and Magnus testing
• Dynamic stability testing

To protect our customers, wind tunnel data is handled with the utmost security. As a government contractor, government-approved policies are in place for protecting proprietary and classified information.  Tunnel access during a test is controlled in accordance with the customer’s instructions.

The HSWT has a wide range of instrumentation capabilities available for testing various types of models.  Our test instrumentation includes a large selection of six-component force and moment balances, five-component flow-through balances, and low-loads rolling moment balances for aerodynamic force and moment testing.  We design, build, and calibrate custom strain gage balances for instrumented control surfaces in-house to offer the highest quality of service to our customers.  Thrust and test stands are available to support propulsion testing. Pressure transducers and pressure scanning modules are available to support inlet and propulsion testing.  High pressure, regulated nitrogen supply is offered to support jet reaction testing.  For a full description of available balances, see Balance Loads and Dimensions.

Digital photography and video recording is included for all test setups and test runs, with shadowgraph imaging available for supersonic test runs.   High speed digital video can be provided for recording high-frequency model dynamics. 

In 2018 a new 3 stage parallel compressor system was installed and it provides 500 psi air at a 50% faster pump rate to the 40,000 ft³ of storage tanks, allowing typical run times from 15 to 110 seconds.  A typical test run consists of 4-5 pitch or roll sweeps.  The remotely controlled model motion cart can provide continuous pitch sweeps from -12 to +22 degrees on the Straight Roll Sting, or -4 to +30 degrees on the Offset Roll Sting, with roll capability from 0 to +360, or 0 +270 degrees, respectively. The High Angle Remote Roll Sting provides selectable pitch ranges of 0 to +30, +30 to +60, or +60 to +90 degrees, and has a full 360 degree roll capability. 

For directions to the HSWT, see the last section of the Facility Handbook.