Consider a rocket carrying 100,000 kg of propellant, 10,000 kg of structure, and 5000 kg of payload.
Recall that the relationship between specific impulse and exhaust velocity is: Vex g*Isp. Assuming that Isp = 450 s and g=9.81 m/s.
what is the value of delta V in m/s that this rocket will produce if all the propellant is consumed in one stage?
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4
Answer:
Explanation:
WHAT IS THE QUESTION???
Answered by
1
Answer:
0.87
0.04
8991.8153
Explanation:
The initial and final masses are:
mi=mprop+mstruct+mpayload
mf=mstruct+mpayload
Substituting these quantities into the Rocket Equation gives:
ΔV=g0 x Isp ln(mi/mf)
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