Aspacecraft approaches jupiter on a hohmann transfer ellipse from the earth. it will fly by jupiter at an altitude of 20,000 km on the sunlit side of the planet. calculate
a. jupiter’s heliocentric velocity
b. the spacecraft’s heliocentric velocity upon arrival at jupiter’s sphere of influence
c. the spacecraft’s hyperbolic excess velocity
d. the eccentricity and turn angle of the hyperbolic flyby trajectory
e. the spacecraft’s heliocentric velocity at the outbound crossing of the sphere of influence. how does it compare to your answer to part b?
f. the angular momentum of the new heliocentric orbit after flyby.

Amass of m 1.5 kg of steam is contained in a closed rigid container. initially the pressure and temperature of the steam are: p 1.5 mpa and t 240°c (superheated state), respectively. then the temperature drops to t2= 100°c as the result of heat transfer to the surroundings. determine: a) quality of the steam at the end of the process, b) heat transfer with the surroundings. for: p1.5 mpa and t 240°c: enthalpy of superheated vapour is 2900 kj/kg, specific volume of superheated vapour is 0. 1483 m/kg, while for t 100°c: enthalpy of saturated liquid water is 419kj/kg, specific volume of saturated liquid water is 0.001043m/kg, enthalpy of saturated vapour is 2676 kj/kg, specific volume of saturated vapour is 1.672 m/kg and pressure is 0.1 mpa.

The higher the astm grain-size number, the coarser the grain is. a)-true b)-false

An ideal otto cycle with air as the working fluid has a compression ratio of 8. the minimum and maximum temperatures in the cycle are 300 k and 1340 k. use constant specific heats at room temperature to determine (a) the amount of heat transferred to the air during the heat- addition kj/kg, (b) the thermal efficiency, and (c) the thermal efficiency of a carnot cycle ope limits. process, in rating between the same temperature