Specifications.

Specifications.

The UJ1672A with its unique airframe, all-electric systems and tailored afterburning jet engines,  ensures ULTRA performance.

General Data

> Pilot only in non-pressurised cockpit​
> Fuselage length / wingspan = 1.4
> Maximum speed sea-level = 1040 km/h
> Maximum thrust / maximum weight > 1
​> Wing anhedral = 3 deg
> Two TB300 turbojet afterburning engines
> Wing leading edge sweep = 25 deg
> Maximum weight / wing area = 200 kg/m2
​> Maximum operating altitude = 30,000 ft
> g load rating = + 8 / - 4

General Data

> One pilot only in non-pressurised cockpit​
> Fuselage length / wingspan = 1.4
> Maximum speed sea-level = 1040 km/h
> Maximum thrust / maximum weight > 1
​> Wing anhedral = 3 deg
> Two TB300 turbojet afterburner engines
> Wing leading edge sweep = 25 deg
> Maximum weight / wing area = 200 kg/m2
​> Maximum operating altitude = 30,000 ft
> g load rating = + 8 / - 4

Comparison Data
Note: The pictures of the UJ1672A shown above in the performance images are for illustrations purposes only. The forward fuselage is not representative of the actual UJ1672A and the actual fuselage is not shown for commercial reasons.

​The information contained on this website is purposely restricted in order to protect the aircraft's unique features and the future strategic commercial direction of Terence Jets. Images have been blocked for this purpose. Individuals and businesses that are interested in this venture will be provided with further information under a non-disclosure agreement. Patent pending on the aircraft design.
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