QueSST Main Design Features

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Questions and Answers

What is the purpose of the extended nose on the QueSST?

  • To enhance maneuverability.
  • To shape the forward shock. (correct)
  • To increase the aircraft's speed.
  • To improve fuel efficiency.

What type of engine does the QueSST use?

  • Pratt & Whitney F100
  • Rolls-Royce Olympus 593
  • GE F4D4 (correct)
  • General Electric J79

What is the function of the fixed canard on the QueSST?

  • To reduce drag at high speeds.
  • To increase lift during takeoff.
  • To provide lateral stability.
  • To provide nose-up trim at the low boom design point. (correct)

What is the purpose of the 'mini T-tail'?

<p>To alternate shock impact to sonic signature (C)</p> Signup and view all the answers

Where does the canopy and ejection seat come from?

<p>T-38 Talon (C)</p> Signup and view all the answers

What is the purpose of the conventional tail?

<p>Low-speed stability and control (A)</p> Signup and view all the answers

What is a design feature of the wings?

<p>Single piece wing skins (D)</p> Signup and view all the answers

What is the 'external/enhanced forward vision system'?

<p>A system that enhances the pilot's forward view (A)</p> Signup and view all the answers

What shields the inlet shock?

<p>Wing (C)</p> Signup and view all the answers

Which of these is a feature of the GE F4D4 engine?

<p>Standard production nozzle (B)</p> Signup and view all the answers

Flashcards

Extended Nose

An extended nose on the aircraft designed to shape the forward shock wave, influencing sonic boom characteristics.

Fixed Canard

Small, wing-like surfaces positioned near the front of the aircraft, used for controlling nose-up trim at lower speeds.

Ejection Seat

Allows pilots to eject for safety

Enhanced Forward Vision System

Enhances the pilot's ability to see forward.

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Inlet Shock Shielded by Wing

These are designed to manage and reduce the impact of inlet shock, positioning the wings to help shield airflow into the engine.

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Conventional Tail

Enhances low-speed handling and ensures stability, particularly during takeoff and landing.

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Mini T-Tail

A tail design that reduces the sonic signature.

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Single Piece Wing Skins

Reduces joints and improves aerodynamic efficiency.

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GE F4D4 Engine

Engine utilizing a standard production nozzle.

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Study Notes

  • QueSST Main Design Features include an extended nose that shapes the forward shock.
  • The aircraft is equipped with a fixed canard for nose-up trim at the low boom design point.
  • The canopy and ejection seat are from a T-38.
  • An external/enhanced forward vision system is implemented.
  • The aircraft contains a GE F4D4 engine with a standard production nozzle.
  • The inlet shock is shielded by the wing.
  • The design incorporates single piece wing skins.
  • A conventional tail provides low-speed stability and control.
  • Alternatively, a mini T-tail alters the shock impact to sonic signature.

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