Jawaharlal Nehru Technological University Hyderabad

Jawaharlal Nehru Technological University Hyderabad B.Tech III Year SPACE PROPULSION Previous Question Paper (February - 2023 - R18)

B.Tech | III Year | III-II | R18 | February - 2023

Answer PaperPaper Code: 156CXMaximum Marks: 75Time: 3 Hours

Note: i) Question paper consists of Part A, Part B. ii) Part A is compulsory, which carries 25 marks. In Part A, Answer all questions. iii) In Part B, Answer any one question from each unit. Each question carries 10 marks and may have a, b as sub questions.

Part A

1a

State the Newtons third law.

2 marks

Answer

Newton's third law of motion states that for every action, there is an equal and opposite reaction. This means that whenever one object exerts a force on a second object, the second object simultaneously exerts a force equal in magnitude and opposite in direction on the first object.

1b

What are the types of orbits?

3 marks

Answer

Orbits are generally classified based on their altitude, inclination, and shape. The primary types include:

  • Low Earth Orbit (LEO): Located at an altitude of approximately 160 to 2,000 km, commonly used for Earth observation and the International Space Station.
  • Medium Earth Orbit (MEO): Situated between LEO and Geostationary orbit, typically at altitudes around 20,000 km, primarily used for navigation satellite constellations like GPS.
  • Geostationary Orbit (GEO): A circular orbit at an altitude of approximately 35,786 km above the equator, where the satellite's orbital period matches Earth's rotation, making it appear stationary relative to a point on the ground.
  • Highly Elliptical Orbit (HEO): Orbits with high eccentricity, such as the Molniya orbit, which allow for extended dwell times over high-latitude regions.
  • Sun-Synchronous Orbit (SSO): A near-polar orbit designed so that the satellite passes over any given point on Earth's surface at the same local solar time.
1c

Define specific impulse of a rocket.

2 marks

Answer

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1d

What are the advantages of air augmented rockets?

3 marks

Answer

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1e

What do you mean by combustion instability?

2 marks

Answer

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1f

What are different types of solid grain configurations?

3 marks

Answer

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1g

What are applications of hybrid propellant rockets?

2 marks

Answer

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1h

What are problems associated with cryogenic engines?

3 marks

Answer

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1i

What is Ion propulsion?

2 marks

Answer

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1j

Mention the types of electric propulsion techniques.

3 marks

Answer

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Part B

2

Brief the history of rockets.

10 marks

Answer

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OR
3

What are the various launch trajectories possible? Explain.

10 marks

Answer

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410 marks
a

De-laval nozzle

5 marks

Answer

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b

Aerospike nozzle

5 marks

Answer

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OR
5

Brief about the static testing of rockets and associated instrumentation.

10 marks

Answer

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6

Explain burning mechanism and related zones, of typical solid rocket motor combustion chamber. (Make use of sketch).

10 marks

Answer

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OR
7

Discuss in detail about grain characterization difficulties and aging of solid rocket motor.

10 marks

Answer

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8

Explain working of liquid rocket engine and its subsystems, with the help of neat diagram.

10 marks

Answer

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OR
9

Explain in detail about the combustion mechanism in hybrid propellant rockets.

10 marks

Answer

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10

Differentiate between electro thermal propulsion and electrostatic propulsion.

10 marks

Answer

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OR
11

With the help of diagram and charts, explain how ion thruster generates impulse.

10 marks

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About this paper

This page contains the solved question paper with answers of SPACE PROPULSION from Jawaharlal Nehru Technological University Hyderabad for B.Tech AE III Year III-II, February - 2023, R18.

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