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OL-AC - Directed Energy

The 704th Test Group Operating Location (704TG/OL-AA) at White Sands Missile Range, New Mexico provides co-located Test and Evaluation (T&E) support for Directed Energy (DE) technology currently under development at the Air Force Research Laboratory Directed Energy (AFRL/RD) Directorate.

Activated June 2006, the 704 TG/OL-AA focuses on developing test concepts, planning, methodology, procedures, and techniques for emerging DE programs. The 704 TG/OL-AA serves as a bridge between Research and Development (R&D) and the Test and Evaluation (T&E) community. It can directly support DE technology still under development while accelerating the transition of DE technology from R&D systems to acquisition ready programs. The T&E engineers work in conjunction with AFRL/RD scientists to better understand system capabilities, providing critical requirements for long term T&E infrastructure planning.

The 704TG/OL-AA does not actively manage a test facility. The T&E engineers utilize all available resources within the test community across all military services. This allows the T&E engineers to recommend the appropriate test resources that best suit the test objectives of any DE program.

704 TG/OL-AA supports both High Power Microwaves (HPM) and High Energy Lasers (HEL) technology.

HPM Active Denial System

Advanced Tactical Laser

Self-Protect High Energy Laser Demonstrator Concept

 

Contacts:
Director (505-846-0837)
T&E Engineer (505-853-8029) 

T&E Engineer (505-846-8653)

704 TG/OL-AA Directed Energy
    

Uses

- Embedded developmental test and evaluation personnel in AFRL's Directed Energy (DE) Directorate.

- Supports Air Force DE priorities.

- Regional DE test support through the White Sands Missile Range Test Team.

Unique Capabilities

- Joint DE test site.

- Ideal geographical location and environment.

- Extensive and specialized test infrastructure.

- Aerial cable site.

- Suburban test environment.

- Holloman's High Speed Test Track.

Developmental test and evaluation (DT&E) personnel are embedded in DoD's Center of Excellence for Directed Energy (DE) -- AFRL's Directed Energy Directorate.

- Provides in-house T&E liaison support to Major Range & Test Facility Base (MRTFB)

- Increases T&E awareness of DE technology.

- Provides test support to AFRL/RD programs.


Supports Air Force DE Priorities

- OSD's DE Test S&T Program.

- DE Technology Transition Council.

- AFMC's DE T&E Consortium.

- Test Planning and Execution

         

Regional DE Test Support through WSMR Test Team

- Army's WASMR and HELSTF.

- Navy's NAVSEA Port Hueneme White Sands Detachment.

- Air Force's 704th Test Group.

- Army Research Laboratory.

- Air Force Research Laboratory Directed Energy Directorate (AFRL/RD)

    

    


Salinas Peak High Altitude Test Site

- Mid-northern WSMR point 9,000 feet MSL.

- 360º azimuth field of view.

- Elevations of 3,500-4,000 ft. AGL.

- Salinas Peak is a major instrumented WSMR telemetry and communications site.

- Surface to unlimited airspace.

- Ideal to conduct passive, active or lethal test against airborne targets.

- Ideal for locating ground-based targets in the valley floor.

    


North Oscura Peak High Altitude Test Site

- Azimuth Field of view 360º.

- Look down angle into valley below -- for ground targets 3-35 miles.

- Restricted unlimited altitude airspace -- for airborne targets up to 120 miles.

- Elevations of 2,500-3,000 ft. AGL.

- Up to 4 test site locations.

- Plenty of power and communications.

- Existing facilities.


Why Test with WSMRs Test Team?

- Ideal geographical location and environment.

- Extensive and specialized test infrastructure.

- State-of-the-art WSMR control center.

- Joint DE Test Site.

- Aerial Cable Site.

- Holloman's High Speed Test Track.

- Suburban test environment at Playas, New Mexico.

- AFRL/RD - DoD's Center of Excellence for DE - Premier DE M&S capability - HEL and HPM infrastructure

- ARL - Electromagnetic Vulnerability Assessment Facility


Point of Contact

Directed Energy
505-853-8029 / DSN 263-8029

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

 

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