Rocket Propulsion Questions and Answers – Liquid Propellant Rocket Engine – Flow and Pressure Balance
This set of Rocket Propulsion MCQs focuses on “Liquid Propellant Rocket Engine – Flow and Pressure Balance”. 1. The oxidiser flow (mo) through the gas generator is ____________ if its flow rate through the pump is 10 kg/s and through the thrust chamber is 5 kg/s. a) 5 kg/s b) 15 kg/s c) 20 kg/s … Read more