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Propellant Combustion: 1500 K, 950 kPa Exit section De = 18 cm Pe = 90 kPa V = 1150 m/s Te = 750 K Propellant

Propellant Combustion: 1500 K, 950 kPa Exit section De = 18 cm Pe = 90 kPa V = 1150 m/s Te = 750 K Propellant

Elements Of Electromagnetics
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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Suppose that the solid-propellant rocket  is
built into a missile of diameter 70 cm and length 4 m. The
system weighs 1800 N, which includes 700 N of propellant.
Neglect air drag. If the missile is fi red vertically from
rest at sea level, estimate ( a ) its velocity and height at fuel
burnout and ( b ) the maximum height it will attain.

Propellant Combustion: 1500 K, 950 kPa Exit section De = 18 cm Pe = 90 kPa V = 1150 m/s Te = 750 K Propellant
Transcribed Image Text:Propellant Combustion: 1500 K, 950 kPa Exit section De = 18 cm Pe = 90 kPa V = 1150 m/s Te = 750 K Propellant
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