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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2021
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Article
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Tab 9
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Research Article
Design Optimization and Parameter Analysis of a Hybrid Rocket Motor-Powered Small LEO Launch Vehicle
Table 9
Payload mass and orbit height of each case.
Case
Payload mass (kg)
Object height (km)
100
300
100
500
100
700
150
300
200
300