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Main Hangar 4802 at Dryden Flight Research Center. NASA photo.| Hangar/Bldg. | Sq. Feet | Availability | Point of Contact |
|---|---|---|---|
| 4801 | 24,300 | 365 days | Tom Grindle, (661) 276-2710 |
| 4802 | 56,230 | 365 days | Tom Grindle, (661) 276-2710 |
| 4820 | 19,680 | As needed | Knut Roepel, (661) 276-3840 |
| 4823 | 6,620 | As needed | Ed Swan, (661) 276-3904 |
| 4826 | 36,430 | 365 days | Tom Grindle, (661) 276-2710 |
| 4833 | 26,010 | Space Shuttle-dependent | Tom Grindle, (661) 276-2710 |
| 4840 | 52,675 | 365 days | Tom Grindle, (661) 276-2710 |
221,945 Total* |
Current Use: Active; science aircraft
Capacities: High bay hangar: 114'D x 152"W x 32'6"H (17,328 ft2) One hangar door located on south side with two 15' drive-through doors, and a 15' drive-through door on north side of building
Unique Capabilities: Office, conference rooms, laboratory, and restrooms. In-floor heating and evaporative cooling. Aircraft air-conditioning system in middle of hangar, AFFF fire system.
Current Use: Active; Support and service/platform medium and small aircraft
Capacities: High bay hangar: 351'D x 152'W x 32'6" H. Two hangar doors, one at south side and one at north side; both with drive-through roll-up doors.
Unique Capabilities: Test areas use portable ground equipment for hydraulics and air systems. AFFF fire system, in-floor heating and evaporative cooling.
Current Use: Active; Load and heat testing of structural components and complete flight vehicles. Calibrate and evaluate flight loads instrumentation under conditions expected in flight.
Capacities: High bay 120'D x 164'W; reinforced concrete floor with tie-down slots in floor and 136'W x 40'H hangar door. Total high bay area 19,680 ft2; 10,000 ft2 useable area for aircraft.
Unique Capabilities: High bay test area with adjacent laboratory, office, and storage area. Data acquisition and test control room overlooking test area. 5-ton rail crane, 39' max height. Carbon-carbon and titanium test capabilities. Thermal and cryogenic systems. Power output range from 1,000 to 20,000 kW and testing temperature range from -100 to 3,000 °F.
Current Use: Active; Aircraft Modification Facility
Capacities: 29800 ft2 (6,624 ft2 hangar space; 72'D x 50'W x 20'H)
Unique Capabilities: Houses Machine Shop, Sheet Metal Shop, Weld Shop, Fluids Shop, Composite Facility, Non-destructive Inspection Shop, and hangar space. Machine Shop is central heating/cooling controlled; other areas are evaporative cooling and radiant heating.
Current Use: Active; houses Avionics Laboratories, research F-15s/F-18 aircraft
Capacities: 25,071 ft2; 192'D x 130'W x 20'H hangar door.
Unique Capabilities: AFFF fire system. Evaporative cooling; has hush houses on outside of building for aircraft hydraulics and cooling units. Normal shop air and 28v DC power.
Current Use: Active; Shuttle Processing Hangar
Capacities: 33,900 ft2 (total)
Unique Capabilities: Water deluge fire system, two 25-ton overhead rail cranes, explosive blow out panels, two exhaust fans, mission control center, communication room, office and laboratory space on north side of building. Two storage areas within hangar. One hangar door on east side of building and one drive-through door on west side of building. Floor drains.
Current Use: Active; research project aircraft
Capacities: Six high bay aircraft test areas; three on each side of building in three physically separated areas.
* Other USAF hangar space potentially available via NASA DFRC/AFFTC Alliance Agreement.