A resistojet has a throat diameter of 0.3 mm and is to be operated with helium at a pressure of 1,000 psi. The exhaust nozzle exit diameter is 3.0 mm. The maximum allowable temperature is 1,000 K and the specific heat ratio of helium can be taken as a constant value of 1.66. Determine the following parameters: 1. The mass flow rate. 2. The specific impulse. 3. The thrust level assuming an isentropic expansion in deep space with zero back pressure.
A resistojet has a throat diameter of 0.3 mm and is to be operated with helium at a pressure of 1,000 psi. The exhaust nozzle exit diameter is 3.0 mm. The maximum allowable temperature is 1,000 K and the specific heat ratio of helium can be taken as a constant value of 1.66. Determine the following parameters: 1. The mass flow rate. 2. The specific impulse. 3. The thrust level assuming an isentropic expansion in deep space with zero back pressure.
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Transcribed Image Text:Question 2:
A resistojet has a throat diameter of 0.3 mm and is to be operated with helium at a pressure of 1,000 psi. The
exhaust nozzle exit diameter is 3.0 mm. The maximum allowable temperature is 1,000 K and the specific heat
ratio of helium can be taken as a constant value of 1.66. Determine the following parameters:
1. The mass flow rate.
2. The specific impulse.
3. The thrust level assuming an isentropic expansion in deep space with zero back pressure.
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