Terence Jets
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Aircraft Type and Features.

The UJ1672A is a high speed subsonic, lightweight, very high performance sport / aerobatic jet aircraft that has a unique shape / configuration. It has similar flying capabilities to a modern military jet fighter while being substantially less complex due to its compact size, simplified low-part-count aircraft structure, simplified flight control system architecture and turbojet powerplant configuration. The UJ1672A has been developed using conventional aerospace design methods and proven technologies to minimise risk and the likelihood of technical difficulties and to ensure it will fly.

Designation

  • The UltraJet™1672A known as the UJ1672A with '1672" representing the birthdate of the aircraft designer Terry Burton and 'A" the first version of the aircraft.

Configuration

  • High wing with large surface area and moderate leading edge sweep, plain trailing edge flaps and ailerons
  • Non-wet fuel tanks
  • Non-pressurised cockpit
  • Retractable landing gear
  • Upswept rear lower fuselage
  • Speed brake on the top aft fuselage
  • Two vertical tails canted outward from the vertical
  • All moving horizontal tailplane
Picture

Flying Controls

  • All-electric flight control system
  • Dual setup for redundancy
Picture

Structure

  • Advanced carbon composite, aluminium, steel, titanium and polycarbonate materials
  • Fuselage of composite sandwich construction with minimal frames
  • Main wing of composite sandwich construction with composite spars
  • Horizontal tailplane and vertical tails of similar construction to the main wing
  • Impact resistant for pilot protection
  • One-piece polycarbonate windscreen
  • Fail safe
Picture
Picture

Powerplant

  • Designated the TB300 with 'TB" representing the name of the engine designer Terry Burton and '300" the 3rd engine design
  • Two custom designed afterburning turbojets as there are no suitable engines available on the market that allow the level of performance desired
  • The TB300 enables a highly tailored engine-airframe integration  
  • Dual electronic control unit (ECU) per engine
  • Designed with simple architecture for increased reliability and safety
  • Variable exhaust nozzle
Picture

Instrumentation

  • Electronic flight instrumentation system (EFIS)
  • ​Basic mechanical backup
Picture

Landing Gear

  • Retractable tricycle with single main wheels and twin nose wheels
  • Nose wheel steerable
  • Landing gear stressed for no flare repetitive landings

Accommodation

  • Single pilot in non-pressurised cockpit
  • Customized carbon fibre pilot support structure
  • Basic pilot emergency egress system

Designation

  • The UltraJet™1672A known as the UJ1672A with '1672" representing the birthdate of the aircraft designer Terry Burton and 'A" the first version of the aircraft.

Configuration

  • High wing with large surface area and moderate leading edge sweep, plain trailing edge flaps and ailerons
  • Non-wet fuel tanks
  • Non-pressurised cockpit
  • Retractable landing gear
  • Upswept rear lower fuselage
  • Speed brake on the top aft fuselage
  • Two vertical tails canted outward from the vertical
  • All moving horizontal tailplane
Picture

Flying Controls

  • All-electric flight control system
  • Dual setup for redundancy
Picture

Structure

  • Advanced carbon composite, aluminium, steel, titanium and polycarbonate materials
  • Fuselage of composite sandwich construction with minimal frames
  • Main wing of composite sandwich construction with composite spars
  • Horizontal tailplane and vertical tails of similar construction to the main wing
  • Impact resistant for pilot protection
  • One-piece polycarbonate windscreen
  • Fail safe
Picture

Powerplant

  • Designated the TB300 with 'TB" representing the name of the engine designer Terry Burton and '300" the 3rd engine design
  • Two custom designed afterburning turbojets as there are no suitable engines available on the market that allow the level of performance desired
  • The TB300 enables a highly tailored engine-airframe integration  
  • Dual electronic control unit (ECU) per engine
  • Designed with simple architecture for increased reliability and safety
  • Variable exhaust nozzle
Picture

Instrumentation

  • Electronic flight instrumentation system (EFIS)
  • ​Basic mechanical backup
Picture

Landing Gear

  • Retractable tricycle with single main wheels and twin nose wheels
  • Nose wheel steerable
  • Landing gear stressed for no flare repetitive landings

Accommodation

  • Single pilot in non-pressurised cockpit
  • Customized carbon fibre pilot support structure
  • Basic pilot emergency egress system

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​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.

Picture
Copyright © 2017 - 2020 Terence Jets Pty Ltd
  • Home
  • Company
  • Venture
    • Introduction
    • History
    • Business Research and Intellectual Property
    • The Potential
    • Innovation
    • The Future
  • The UJ1672A
    • Top Secret
    • Aircraft Type and Features
    • Design
    • Specifications
    • Safety
  • Other Markets
    • Private Aviation
    • Defence
    • Propulsion
    • Further Opportunities
  • Founder
    • Terry Burton
  • Join
    • Positions Vacant
    • Sponsorship
  • Media
  • FAQ
  • Contact