Flat Wing Area
15.7935 m²
Entry Into service
1961-03-17
Maximum Take-Off Weight
5.4853 t (paragliders: kg)
Maximum Range
1835.332 km
Pictures
No pictures yet for this family.
Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Northrop T-38 Talon |
5.4853 |
1835.332 |
Similar airplanes
All data (26 fields)
- Name
- Northrop T-38 Talon
- Manufacturer
- Northrop Corporation
- Description
- The Northrop T-38 Talon is a two-seat, twinjet supersonic jet trainer designed and produced by the American aircraft manufacturer Northrop Corporation.
- ICAO Code
- T38
- First Flight
- 1959-04-10
- Entry Into service
- 1961-03-17
- Production End
- 1972-01-01
- Designer
- Northrop Corporation
- Type
- Advanced trainer
- Length (m)
- 14.0208
- Height (m)
- 3.6576
- Cockpit Crew
- 2
- Max Speed (km/h)
- 1381.591
- Max Ceiling (m)
- 15240
- Rate of Climb (m/s)
- 170.688
- Max Mach (Mach)
- 1.3
- National Origin
- United States of America
- Number Built
- 1187
- Powerplant Description
- 2 × General Electric J85-5A afterburning turbojet engines
- Primary Users
- United States Air Force, United States Navy, NASA, Turkish Air Force
- Status
- Operational
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Northrop_T-38_Talon
- Flat Wing Span (m)
- 7.62
- Flat Wing Area (m²)
- 15.7935
- Wake Category
- L
- Number of Engines
- 2