Fact Sheet Display

MARK 1 TEST FACILITY

The Mark 1 Test Facility is a state-of-the-art space environment simulation test chamber for full-scale space systems testing. A $1.5 million dollar upgrade in fiscal year 2000 replaced existing oil diffusion pumps with a complete dry pumping system, cleaned the interior of the chamber and refinished the surface the (LN2) thermal shroud. A new Hewlett Packard 3852, with 1,500 channels of data capability, replaced the previous Micro-Vax data system. These upgrades, combined with the shear size of the facility, at 42-foot-diameter by 82-foot, postures AEDC for future testing of full-scale satellites and other space systems requiring a contamination-free test environment. 


CAPABILITIES
Thermal: Chamber is completely lined with a liquid nitrogen shroud that can provide thermal conditions down to 77 degrees Kelvin. 
Vacuum Range: ≤ 5x10-7 Torr to local atmospheric pressure. 
Working Volume: 36 foot diameter x 70 foot tall. 
Support Structure: 200,000 pounds /12-foot-square seismic mass provides vibration isolated of test articles. 
Pumping System: Mechanical roughing pumps, turbo molecular and cryogenic high vacuum pumps, all with cryogenic traps. 
Loading: Vertical: 20-foot opening in top of chamber, via a 15-ton precision crane. Horizontal: 8-foot diameter manway in the chamber side near the bottom. 
Cold Wall: Lined with 77 degrees Kelvin liquid nitrogen, cryogenic shroud. 
Special Features: Laminar flow optical quality clean room (400 square foot, better than Class 1000). 15-ton precision crane. 
Data: All facility data time tagged and archived. 1,500 channel test data system available. 
Work Areas: Test customer offices available. Limited hardware storage available. Two large bay areas available for test article build-up. 
Solar Simulation: Infrared lamp arrays available for thermal cycling. 
Other: 15 degrees Kelvin gaseous helium cryopumping capability available.

LANDING GEAR TEST FACILITY

Overview

The Landing Gear Test Facility (LGTF) has been a cornerstone of aerospace testing at Wright-Patterson Air Force Base since 1942, dedicated to ensuring the reliability and performance of aircraft landing gear systems.

Throughout its history, the LGTF has supported the warfighter by providing critical data to enhance the safety and effectiveness of landing gear, wheels, tires, and brakes, directly contributing to the mission of the United States Department of Defense. In addition to its military focus, the LGTF offers comprehensive testing services to commercial entities, employing world-unique test machines capable of simulating real-life conditions with unparalleled accuracy.

Guided by the core values of IntegrityService, and Excellence, the LGTF consistently delivers precise and dependable data to both military and commercial partners.

Test Machine Capabilities

 

 Overall System Specifications:

Max Speed: 250 mph
Max Acceleration: 21 ft/s2
Inertial Equivalent: 2,445 - 20,063 lbs.
Max Kinetic Energy: 41,750,000 ft-lbs.

 

South Carriage Specifications:

Max Load: 40,000 lbs.
Max Torque: 375,000 in-lbs.
Max Tire Size: 64 in

 

North Carriage Specifications:

Max Load: 25,000 lbs.
Max Torque: 72,000 in-lbs.
Max Tire Size: 48 in

Overall System Specifications:

Max Speed: 350 mph
Max Acceleration: 24 ft/s2

South Carriage Specifications:

Max Load: 150,000 lbs.
Max Yaw: ± 20°
Max Camber: ± 20°

North Carriage Specifications:

Max Load: 100,000 lbs.

 

Overall System Specifications:

Max Speed: 200 mph
Max Acceleration: 2 ft/s2
Inertial Equivalent: 10,147 - 162,987 lbs.
Max Kinetic Energy: 205,000,000 ft-lbs.

South Carriage Specifications:

Max Load: 301,500 lbs.
Max Brake Torque: 5,800,000 in-lbs.

Overall System Specifications:

Max Speed: 250 mph
Max Acceleration: 16 ft/s2
Max Vertical Load: 150,000 lbs.
Max Yaw: ± 20°
Max Camber: ± 10°

Overall System Specifications:

Max Compressive Load: 3,000,000 lbs.
Max Tension Load: 1,000,000 lbs.
Max Stroke: 60 in
Max Height: 28 ft
Max Width: 10 ft
Platen Size: 60.5 x 96 in

Overall System Specifications:

Max Vertical Load: 75,000 lbs.
Max Side Load: 30,000 lbs.
Max Yaw: ± 90°
Max Camber: ± 10°
Max Tire Size: 56 in.
Table Length: 20 ft.
Max Travel Speed: 3 in/s
Roll Distance: 217 in

 

Overall System Specifications:

Below-grade safety enclosure
Dimensions: 72 x 120 x 126 in.
Water Pressure Limit: 5,000 psi
Rate of Inflation: 10 psi/min

Drop Tower #1

Load Range: 750 - 3,600 lbs.
Wing Lift: 200 - 3,600 lbs.

 

Drop Tower #2

Load Range: 2,000 - 10,300 lbs.
Wing Lift: 200 - 10,300 lbs.

 

Drop Tower #3

Load Range: 6,500 - 50,000 lbs.
Wing Lift: 200 - 35,000 lbs.

 

Drop Tower #4

Load Range: 35,000 - 150,000 lbs.
Wing Lift: 200 - 150,000 lbs.

Load frame that accommodates multiple hydraulic cylinders to provide controlled forcing and operational stresses to test objects in all 6 axes.

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CONTACT US

704 TG/OL-ACL
Landing Gear Test Facility
1981 5th Street
Area B, Bldg. 31
Wright-Patterson AFB, OH 45433
(937) 255-9216
704.tg.olac@us.af.mil

 

WHERE TO FIND US

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