For cold gas propellants, tank pressure is typically between and

100 Mpa; 500 Mpa

200 Mpa; 1000 Mpa

300 Mpa; 500 Mpa

300 Mpa; 1000 Mpa

Correct Answer : 300 Mpa; 1000 Mpa

Explanation : The tank used for the storage of cold gas propellants typically have a pressure between 300 Mpa and 1000 Mpa. Cold gas propulsion is used typically for low thrust space propulsion purposes. Nitrogen is the most preferred cold gas propellant due to its lack of contamination, storage density and performance characteristics.

Recently Updated in Rocket Propulsion Questions

Use of solenoid valves increases power consumption for a cold gas propellant system.

True

False

Can Not Say

None of the above

Correct Answer : Option (B) : False

Explanation : In order to decrease power consumption, one can use solenoid valves. It requires an electric pulse to open and close and hence can be easily controlled with lesser power expended.

For a short period of operation (lasting few minutes), the gas expansion in cold gas systems is ________

adiabatic

isothermal

homogenous

heterogeneous

Correct Answer : Option (A) : adiabatic

Explanation : Since the operation lasts only a short period of time, the expansion can be taken as adiabatic. It means that there is no heat absorption or release by the gas.

Thrust in RCS is produced by the momentum exchange between exhaust and the _______

pump

injector

payload

spacecraft

Correct Answer : Option (D) : spacecraft

Explanation : Thrust generation is due to the exchange of momentum between exhaust and the spacecraft. The thrust is given by Newton’s second law F = mV_e.