The Development of the F35 Joint Strike Fighter: A Next Generation Military Aircraft

The Development of the F35 Joint Strike Fighter: A Next Generation Military Aircraft

Assessment

Interactive Video

Architecture, Other, Social Studies

KG - University

Hard

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The transcript discusses the development of a new generation of fighter aircraft by Lockheed Martin, which will replace current models. The aircraft will be produced in three variants: conventional, naval, and short takeoff/vertical landing. The F136 engine, developed by GE and Rolls Royce, is central to the aircraft's design. The Stovel engine system, a key innovation, includes a lift band for vertical lift. The naval version of the aircraft features enhanced structures for carrier operations.

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5 questions

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1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What are the three variants of the next generation fighter aircraft being developed by Lockheed Martin?

Conventional takeoff and landing, naval, and short takeoff and vertical landing

Conventional takeoff and landing, stealth, and supersonic

Naval, stealth, and supersonic

Short takeoff and vertical landing, stealth, and supersonic

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which companies are developing the F136 engine for the next generation fighter aircraft?

Lockheed Martin and Boeing

GE and Rolls Royce

Airbus and GE

Rolls Royce and Boeing

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How many engines are planned for production and qualification during the system development phase?

16 engines

14 engines

12 engines

10 engines

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the purpose of the shaft-driven lift fan developed by Lockheed Martin?

To provide horizontal thrust

To enhance stealth capabilities

To provide cool air thrust for vertical lift

To increase supersonic speed

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What modifications are made to the naval version of the F35 to handle carrier operations?

Smaller wing and tail control surfaces, and stronger internal structure

Larger wing and tail control surfaces, and lighter internal structure

Smaller wing and tail control surfaces, and lighter internal structure

Larger wing and tail control surfaces, and stronger internal structure