EAGLE AVIATION TECHNOLOGIES LLC
NEWPORT NEWS, VIRGINIA 236071517
Top Industries (NAICS)
| NAICS Code | Obligations | Awards |
|---|---|---|
| 541715 | $3.71M | 28 |
| 332999 | $26K | 2 |
Contract Awards
13 awards found
DESIGN, ANALYSIS, AND FABRICATION OF THE TILT WING TEST RIG. A POWERED, SEMI-SPAN WIND TUNNEL MODEL THAT WILL BE TESTED AT NASA LANGLEY'S SUBSONIC WIND TUNNEL IN THE WALLS-DOWN, OPEN JET SMOOTH FLOOR, AND OPEN JET ACOUSTICS FLOOR CONFIGURATIONS.
DESIGN, ANALYSIS, AND FABRICATION OF THE TILT WING TEST RIG. A POWERED, SEMI-SPAN WIND TUNNEL MODEL THAT WILL BE TESTED AT NASA LANGLEY'S SUBSONIC WIND TUNNEL IN THE WALLS-DOWN, OPEN JET SMOOTH FLOOR, AND OPEN JET ACOUSTICS FLOOR CONFIGURATIONS.
FABRICATION OF A DOGLEG STING FOR TESTING IN THE NASA LANGLEY RESEARCH CENTER (LARC) 31-INCH MACH 10 TUNNEL (31M10) IN SUPPORT OF THE VULCAN ENGINE RECOVERY AEROSHELL (VERA) PROJECT.
FLAT COMPOSITE PANELS FOR IMPACT TESTING
DESIGN, ANALYSIS, AND FABRICATION OF THE TILT WING TEST RIG. A POWERED, SEMI-SPAN WIND TUNNEL MODEL THAT WILL BE TESTED AT NASA LANGLEY'S SUBSONIC WIND TUNNEL IN THE WALLS-DOWN, OPEN JET SMOOTH FLOOR, AND OPEN JET ACOUSTICS FLOOR CONFIGURATIONS.
RELIANCE CONSOLIDATED MODELS VI MINIMUM GUARANTEE DELIVERY ORDER.
DESIGN, ANALYSIS, AND FABRICATION OF THE TILT WING TEST RIG. A POWERED, SEMI-SPAN WIND TUNNEL MODEL THAT WILL BE TESTED AT NASA LANGLEY'S SUBSONIC WIND TUNNEL IN THE WALLS-DOWN, OPEN JET SMOOTH FLOOR, AND OPEN JET ACOUSTICS FLOOR CONFIGURATIONS.
DESIGN AND FABRICATION TO REPAIR AND UPGRADE THE TILTROTOR AEROELASTIC STABILITY TESTBED WIND-TUNNEL MODEL FOR THE SECOND ENTRY INTO THE TRANSONIC DYNAMICS TUNNEL.
DESIGN, ANALYSIS AND FABRICATION OF A NEW VACUUM SPIN STAND SUITABLE FOR TESTING ROTOR BLADES INSIDE THE NASA LANGLEY RESEARCH CENTER'S LANGLEY AEROTHERMODYNAMICS LABORATORY (LAL) 60-FT VACUUM SPHERE TEST CHAMBER (60VSTC).
COMPOSITE PANELS FOR IMPACT TESTING.
DESIGN AND FABRICATION TO REPAIR AND UPGRADE THE TILTROTOR AEROELASTIC STABILITY TESTBED (TRAST) WIND-TUNNEL MODEL FOR THE SECOND ENTRY INTO THE TRANSONIC DYNAMICS TUNNEL (TDT).
FABRICATION OF A COMPOSITE BASED FUSELAGE STRUCTURE OF THE NASA RVLT LIFT+CRUISE CONCEPT VEHICLE. ALLOWS FOR VEHICLE LEVEL IMPACT TESTS TO BE CONDUCTED FOR THE GENERATION OF CRASHWORTHINESS PERFORMANCE AND OCCUPANT INJURY RISK DATA
DESIGN, ANALYSIS, AND FABRICATION OF A HELICOPTER FUSELAGE, WINGS, AND A TAIL ASSEMBLY FOR WIND TUNNEL TESTING.
Business Details
- UEI
- CTGLCH53ZYZ9
- CAGE Code
- 5TP12
- Address
- 7505 WARWICK BLVD
NEWPORT NEWS, VA 236071517 - Congressional District
- VA-03
- Phone
- 7572620445
Parent Company
EAGLE AVIATION TECHNOLOGIES LLC
Data Source
This profile is based on federal contract award data from USAspending.gov.
View on USAspending.gov