Roll No.
Total No. of Pages : 02
Total No. of Questions : 09
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B.Tech.(Aerospace Engg.) (2012 Batch) (Sem.–6)
SATELLITES AND SPACE SYSTEM DESIGNS
Subject Code : ASPE-310
M.Code : 72455
Time : 3 Hrs. Max. Marks : 60
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INSTRUCTIONS TO CANDIDATES:
- SECTION-A is COMPULSORY consisting of TEN questions carrying TWO marks each.
- SECTION-B contains FIVE questions carrying FIVE marks each and students have to attempt any FOUR questions.
- SECTION-C contains THREE questions carrying TEN marks each and students have to attempt any TWO questions.
SECTION–A
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- Write briefly:
- Ionization decay decreases as___________density falls.
- What is a space mission?
- What is a stereo configuration?
- Name two mid launch phenomenon.
- What is the operating temperature of infrared sensors?
- What is the work done by system when spacecraft is in flight?
- Name any two thermal control hardware used.
- What is the use of Louvers?
- What is the approximate sensing method for spacecraft attitude?
- What is a thermal balance test?
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SECTION-B
- Explain preliminary design review of a space craft.
- Describe the importance of space mission life cycle.
- What are the factors responsible for thermal design of space craft?
- What is the role of mission operator center?
- Explain spacecraft integration.
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SECTION-C
- What do you mean by reliability? What are the assumptions in the reliability statement? Assume we have an n-component system. We usually have a choice of providing redundant components or of providing a totally redundant system. How do these two levels of redundancy compare? Assume each component has the same level of reliability, R.
- What is a mock up? Why it is made? Explain different system mockups of a spacecraft.
- What are the main considerations of a launch vehicle? Describe thermal technology.
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