Rocket Propulsion Questions and Answers – Thrust Chambers – Heat Transfer Analysis

This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Thrust Chambers – Heat Transfer Analysis”. 1. If dT/dL denotes temperature gradient with respect to thickness L at the surface A, k denotes the thermal conductivity, then the heat transferred per unit area is given by __________ a) Q/A = -k dT/dL … Read more

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Rocket Propulsion Questions and Answers – Thrust Chambers – Combustion Chamber and Nozzle

This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Thrust Chambers – Combustion Chamber and Nozzle”. 1. Burning of the propellants take place in __________ a) nozzle b) injector c) combustion chamber d) engine casing 2. The volume of the combustion chamber is selected on the basis of which of these … Read more

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Rocket Propulsion Questions and Answers – Thrust Chambers – Injectors

This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Thrust Chambers – Injectors”. 1. The carburetor of an internal combustion engine has a similar function as __________ a) injector b) thrust chamber c) nozzle d) propellant tank 2. The process by which liquids are broken into small droplets is called __________ … Read more

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Rocket Propulsion Questions and Answers – Gaseous Propellants

This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Gaseous Propellants”. 1. Which of the following is not a gold gas propellant? a) Nitrogen b) Argon c) Freon 14 d) Hydrazine 2. For cold gas propellants, tank pressure is typically between __________ and __________ a) 300 Mpa; 1000 Mpa b) 100 … Read more

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Rocket Propulsion Questions and Answers – Liquid Monopropellants

This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Liquid Monopropellants”. 1. Which of the following is a monopropellant? a) H2 b) Diluted H2O2 c) Hydrazine d) Monomethyl hydrazine 2. ___________ is not a method of monopropellant ignition. a) Flame heat b) Electrical c) Catalytic material d) Pulverization 3. ___________ is … Read more

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Rocket Propulsion Questions and Answers – Liquid Fuels

This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Liquid Fuels”. 1. __________ is not liquid fuel. a) Xylidine b) Furfuryl alcohol c) Hydrazine hydrate d) Nitric acid 2. Which of the following is not a liquid fuel? a) Ammonia b) Ethyl alcohol c) Borohydrides d) Hydrogen peroxide 3. Petroleum derivatives … Read more

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Rocket Propulsion Questions and Answers – Liquid Oxidizers

This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Liquid Oxidizers”. 1. __________ are not liquid oxidizers. a) Nitrogen-fluorine formulations b) Oxygen-fluorine compounds c) Fluorinated hydrocarbons d) Borohydrides 2. ___________ is a commonly used liquid oxidizer. a) ClF3 b) OF2 c) ClF5 d) H2O2 3. LOX boils at _______ atmospheric pressure. … Read more

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Rocket Propulsion Questions and Answers – Propellant Properties

This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Propellant Properties”. 1. Which of the following propellants were used in the Titan mission? a) 50% UDMH + 50% hydrazine b) RP1 c) RDX d) Aviation gasoline 2. Which of the following is not a factor considered in the selection of liquid … Read more

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Rocket Propulsion Questions and Answers – Liquid Propellant Rocket Engine – Valves and Pipelines

This set of Rocket Propulsion Objective Questions & Answers focuses on “Liquid Propellant Rocket Engine – Valves and Pipelines”. 1. When these valves are shut, it shuts off a portion of the propulsion system _________ a) burst diaphragm b) isolation valves c) control valves d) drainage valves 2. Two valves commonly used in pressurized feed … Read more

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Rocket Propulsion Questions and Answers – Rocket Engines for Manueuvering, Orbit Adjustments, or Attitude Control

This set of Rocket Propulsion MCQs focuses on “Rocket Engines for Manueuvering, Orbit Adjustments or Attitude Control”. 1. What is the nature of thrusters and feed system for attitude control rocket engines? a) small; common pressurized feed system b) large; separate turbopump feed system c) small; separate pressurized feed system d) large; common turbopump feed … Read more

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Manish Bhojasia - Founder & CTO at Sanfoundry
Manish Bhojasia, a technology veteran with 20+ years @ Cisco & Wipro, is Founder and CTO at Sanfoundry. He lives in Bangalore, and focuses on development of Linux Kernel, SAN Technologies, Advanced C, Data Structures & Alogrithms. Stay connected with him at LinkedIn.

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