Engineering, 30.08.2019 02:10 greend0719
Design a solid or hybrid upper stage propulsion module (pm) with the capability to boost a 181 kg payload from a 352 km circular orbit to a 704 km circular orbit. of the 181 kg payload, 125 kg is allocated for the experimental satellite, leaving no more than 56 kg for the pm. show your design’s a) throat area b) exit area c) exhaust velocity d) mass flow rate state any assumptions that you make. hint, it takes 0.52 m/s to raise the orbit 1 km at an altitude of 352 km.
Answers: 1
Engineering, 04.07.2019 18:10
Acompressor receives the shaft work to decrease the pressure of the fluid. a)- true b)- false
Answers: 3
Engineering, 04.07.2019 18:10
Water at 70°f and streams enter the mixing chamber at the same mass flow rate, determine the temperature and the quality of the exiting stream. 0 psia is heated in a chamber by mixing it with saturated water vapor at 20 psia. if both streams enters the mixing chamber at the same mass flow rate, determine the temperature and the quality of the existing system.
Answers: 2
Engineering, 04.07.2019 18:10
Adouble-strand no. 60 roller chain is used to transmit power between a 13-tooth driving sprocket rotating at 300 rev/min and a 52-tooth driven sprocket. a) what is the allowable horsepower of this drive? b) estimate the center-to-center distance if the chain length is 82 pitches. c) estimate the torque and bending force on the driving shaft by the chain if the actual horsepower transmitted is 30 percent less than the corrected (allowable) power.
Answers: 3
Engineering, 04.07.2019 18:10
A-mn has a cubic structure with a0 0.8931 nm and a density of 7.47 g/cm3. b-mn has a different cubic structure, with a0 0.6326 nm and a density of 7.26 g/cm3. the atomic weight of manganese is 54.938 g/mol and the atomic radius is 0.112 nm. determine the percent volume change that would occur if a-mn transforms to b-mn.
Answers: 2
Design a solid or hybrid upper stage propulsion module (pm) with the capability to boost a 181 kg pa...
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