Answer to Question #150959 in Mechanical Engineering for Yogendra Shivankar

Question #150959
A classic hybrid propulsion system has the following characteristics:

Propellants: HTPB/LOX

Nominal Burn Time: 20 Seconds

Initial Chamber Pressure: 600psi

Initial mixture ratio: 2.0

Initial nozzle exit area ratio: 10

Fuel grain outside dia: 12in

Grain Geometry: Single cylinder case bonded

Initial HTPB Temp: 65F

Determine:

-Initial and Final Thrust

-Specific Impulse

-Propellant Masses

-Useful Propellant
1
Expert's answer
2020-12-22T05:01:38-0500
Dear Yogendra Shivankar, your question requires a lot of work, which neither of our experts is ready to perform for free. We advise you to convert it to a fully qualified order and we will try to help you. Please click the link below to proceed: Submit order

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