Engineering Questions with Answers - Multiple Choice Questions

Rocket Propulsion – Liquid Oxidizers

1 - Question

__________ are not liquid oxidizers.
a) Nitrogen-fluorine formulations
b) Oxygen-fluorine compounds
c) Fluorinated hydrocarbons
d) Borohydrides
View Answer Answer: d
Explanation: Borohydrides are not liquid oxidizers. Rest of the options are storable, cryogenic liquid oxidizer propellants with high specific impulse values.



2 - Question

___________ is a commonly used liquid oxidizer.
a) ClF3
b) OF2
c) ClF5
d) H2O2
View Answer Answer: d
Explanation: Hydrogen peroxide (H2O2) is a commonly used liquid oxidizer. But ClF2, OF2, ClF5, etc. are experimental liquid oxidizers.



3 - Question

LOX boils at _______ atmospheric pressure.
a) 909C
b) 90 K
c) 90 F
d) 90 R
View Answer Answer: b
Explanation: LOX refers to liquid oxygen. It boils at 90 K. Since their boiling point is very low, a cryogenic setup is required for the storage and transport of this oxidizer.



4 - Question

Which of the following is the specific gravity and heat of vaporization of LOX at atmospheric pressure?
a) 1.14; 213 kJ/kg
b) 1.08; 253 kJ/kg
c) 1.80; 235 kJ/kg
d) 1.41; 231 kJ/kg
View Answer Answer: a
Explanation: LOX refers to liquid oxygen. It has a specific gravity of 1.14. That means it is 1.14 times denser than water having a density of about 1000 kg/m3. It has a heat of vaporization of 213 kJ/kg.



5 - Question

What is the decrease in specific gravity of LOX if the tank pressure is increased from atmospheric pressure to 8 atm? (At 8 atm, specific gravity of LOX is 0.88)
a) 32.3%
b) 28.2 %
c) 22.8%
d) 25.3%
View Answer Answer: c
Explanation: The increase can be calculated using δinc = (δnew – δold) / δold x 100. δinc=(0.88-1.14)/1.14 x 100 = -22.8. Hence the decrease is 22.8%.



6 - Question

When are the tanks with cryogenic propellants pressurized?
a) Just before the engine start
b) After the engine start
c) 10 sec after the engine start
d) 10 sec before the engine start
View Answer Answer: a
Explanation: This is done to ensure that the propellants are at its lowest possible temperature. Else they might evaporate within the tank and may lead to devastating results under wrong circumstances.



7 - Question

Which of the following percentages of concentration of hydrogen peroxide is used for rocket applications?
a) 80 %
b) 60 %
c) 30 %
d) 10 %
View Answer Answer: a
Explanation: H2O2 used for rocket applications has a concentration of 80%. It is said to be in its highly concentrated form from 70% to 99%. For commercial uses, hydrogen peroxide is available at 30% concentration.



8 - Question

In the combustion chamber, hydrogen peroxide decomposes to give __________
a) hydrogen and oxygen
b) hydrogen and water
c) oxygen and water
d) water
View Answer Answer: c
Explanation: Decomposition of hydrogen peroxide gives oxygen and water. The reaction is represented as H2O2 → H2O + 1/2O2 + heat.



9 - Question

Which of the following is not a catalyst used for H2O2 decomposition?
a) Platinum
b) Iron oxide
c) Manganese dioxide
d) Aluminium
View Answer Answer: d
Explanation: Aluminium tanks are generally used for storing H2O2 for this reason. Whereas hydrazine is not compatible with iron, copper, its alloys, monel, magnesium, zine or some types of aluminium alloys.



10 - Question

Theoretical specific impulse of 90% H2O2 is _______
a) 204 s
b) 154 s
c) 321 s
d) 114 s
View Answer Answer: b
Explanation: 90% H2O2 has a specific impulse of 204s. Because of this good specific impulse, countries like USA, Russia and Germany used concentrated hydrogen peroxide for monopropellant gas generation before 1955.

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