JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD

JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech IV LAUNCH VEHICLE AND MISSILE TECHNOLOGY Previous Question Paper (September - 2020 - R15)

B.Tech | IV | IV-II | R15 | September - 2020

Answer PaperPaper Code: 128CMMaximum Marks: 75Time: 2 hours

Answer any Five Questions
All Questions Carry Equal Marks

Main

115 marks
a

Write a short note on similarities and differences in rockets and missiles.

7 marks

Answer

Both rockets and missiles rely on the principle of Newton's Third Law of Motion, utilizing high-velocity exhaust gases generated by internal combustion to produce thrust. They share fundamental subsystems, including propulsion systems (solid or liquid propellant engines), airframes, and aerodynamic control surfaces for stability during flight.

The primary differences lie in their purpose and guidance: a rocket is generally an unguided vehicle used for space launch or artillery, where the trajectory is determined by the initial launch angle and gravity. In contrast, a missile is a precision-guided weapon system equipped with an onboard guidance, navigation, and control (GNC) system, allowing it to adjust its flight path in real-time to intercept a moving or static target. Furthermore, missiles incorporate a payload section specifically designed as a warhead with fusing mechanisms, whereas rockets typically carry scientific instruments or satellites.

b

Mention some of the criteria’s in the selection of materials for launch vehicles.

8 marks

Answer

The selection of materials for launch vehicles is critical due to the extreme environments encountered during ascent. Key criteria include:

  • High Strength-to-Weight Ratio: Materials must be lightweight to maximize payload capacity while possessing sufficient structural integrity to withstand high aerodynamic loads and internal pressure.
  • Thermal Stability: Materials must resist extreme temperature fluctuations, from cryogenic temperatures of liquid propellants to the intense aerodynamic heating during atmospheric re-entry or high-speed flight.
  • Fracture Toughness and Fatigue Resistance: The material must resist crack propagation and cyclic loading stresses experienced during engine ignition, vibration, and acoustic loading.
  • Corrosion Resistance: Compatibility with propellants, such as liquid oxygen or hypergolic fuels, is essential to prevent chemical degradation of tanks and plumbing.
  • Fabricability: The ability to be machined, welded, or formed into complex geometries like thin-walled pressure vessels is vital for cost-effective manufacturing.
  • Low Thermal Expansion: Maintaining dimensional stability under varying thermal loads is necessary to ensure the alignment of sensitive guidance and control components.
215 marks
a

Discuss briefly propulsion system used in missiles.

7 marks

Answer

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b

Explain the need of control and guidance of missiles.

8 marks

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315 marks
a

Describe the principal features of solid propellant rocket.

7 marks

Answer

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b

What properties of solid propellant improve the performance?

8 marks

Answer

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415 marks
a

What is propellant grain and how its design effects the performance of rocket.

7 marks

Answer

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b

Which type of injectors are used in liquid propellant rockets.

8 marks

Answer

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5

Explain about lateral aerodynamic, lateral damping and longitudinal moments of a rocket.

15 marks

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615 marks
a

Write a short note on rocket dispersion and its need.

7 marks

Answer

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b

What are the design considerations for re-entry vehicles?

8 marks

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715 marks
a

Discuss about stage separation dynamics.

7 marks

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b

Mention different types of thrust vector mechanisms with neat sketches.

8 marks

Answer

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8

Explain the instrumentation and data management systems used in rocket testing.

15 marks

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About this paper

This page contains the question paper of LAUNCH VEHICLE AND MISSILE TECHNOLOGY from JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD for B.Tech AE IV IV-II, September - 2020, R15.

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