Podcast
Questions and Answers
Which design feature is primarily responsible for generating a forward shock on the QueSST aircraft?
Which design feature is primarily responsible for generating a forward shock on the QueSST aircraft?
- Mini T-tail
- Extended Nose (correct)
- GE F4D4 Nozzle
- Conventional Tail
What is the purpose of the fixed canard on the QueSST aircraft?
What is the purpose of the fixed canard on the QueSST aircraft?
- Enhancing low-speed stability
- Maintaining nose-up trim at low speeds (correct)
- Minimizing sonic signature
- Providing a rearward shock
Which of the following design features is not directly related to minimizing sonic signature or improving aerodynamic performance?
Which of the following design features is not directly related to minimizing sonic signature or improving aerodynamic performance?
- Canopy and Ejection Seat (correct)
- Conventional Tail
- Single Piece Wing Skins
- Inlet Shock Shielded by Wing
Which of the following design aspects contributes most significantly to the aircraft's low-speed handling and stability?
Which of the following design aspects contributes most significantly to the aircraft's low-speed handling and stability?
Which of the following design elements is NOT explicitly mentioned as being derived from another aircraft?
Which of the following design elements is NOT explicitly mentioned as being derived from another aircraft?
Flashcards
Extended Nose
Extended Nose
A forward shock-inducing shape at the nose of the aircraft.
Fixed Canard
Fixed Canard
A horizontal surface used for maintaining nose-up trim at low speeds, set at the boom design point.
GE F4D4 Nozzle
GE F4D4 Nozzle
The standard engine nozzle used in the QueSST aircraft for propulsion.
Mini T-tail
Mini T-tail
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Single Piece Wing Skins
Single Piece Wing Skins
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Study Notes
QueSST Design Features
- The aircraft has a fixed canard for nose-up trim at low speeds
- The aircraft's nose shape creates a forward shock
- The aircraft uses a GE F4D4 engine with a standard production nozzle
- A T-38 ejection seat and canopy are included
- A mini T-tail design is used to reduce sonic signature
- Conventional tail design is available for low-speed stability and control
- A single piece wing skin is used
- The aircraft features an external/enhanced forward vision system for the pilot
- Inlet shock is shielded by the wing
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