subject
Physics, 16.02.2021 01:40 briannawoods13

A chemical rocket is used for launch into earth orbit. At the end of the combustion chamber the stagnation temperature is 3000 K. The molecular weight of the combustion products is 26. The gases expand isentropically as an ideal gas mixture with specific-heat ratio 1.2. The area ratio Ae/A* of the nozzle is 20, and the throat diameter is 0.1 m. Determine: a. The stagnation pressure if the expansion is correct at sea level; b. The rocket thrust at sea level, 15-km, 30-km, and 60-km altitude

ansver
Answers: 1

Another question on Physics

question
Physics, 22.06.2019 07:30
Choose all the answers that apply. our solar system: is in a spiral galaxy no longer includes pluto is made mostly of empty space is in the andromeda galaxy is the only known system that supports life
Answers: 3
question
Physics, 22.06.2019 09:10
The diagram shows a series of volcanic island and a hot spot determine the direction of movement of the tectonic plate that for the island
Answers: 2
question
Physics, 22.06.2019 19:00
Why do different substances have diffrent properties
Answers: 1
question
Physics, 22.06.2019 21:30
What ia the energy of an object because of its potential and kinetic energies
Answers: 1
You know the right answer?
A chemical rocket is used for launch into earth orbit. At the end of the combustion chamber the stag...
Questions
question
Mathematics, 01.08.2019 00:30