Introduction to Rocket Science and Engineering
Citations
5 citations
Cites background from "Introduction to Rocket Science and ..."
...For sounding rockets, typical values for thrust-to-weight ratio is within the range of 3-4 (Taylor, 2009): 705.3 , 9.8 avg w L Thrust T Weight m = = × (1) where, mL is the lift off mass of the rocket....
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3 citations
Cites background from "Introduction to Rocket Science and ..."
...Ullman (1992) describes the relationship as: 9 = Strong Relation 3 = Medium Relation 1 = Weak Relation Blank = No Relation The relationship of customer requirements to both engineering performance specifications and geometry and description specifications is attached at appendix C6-1 and C6-2 respectively....
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3 citations
3 citations
Cites methods from "Introduction to Rocket Science and ..."
...Escape from the planet The Tsiolkovsky equation [7, 8] gives the maximum change in velocity (delta-V) applicable to a simple single stage rocket or a single stage in a multistage rocket: (1)...
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