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Rocket Propulsion Study guides, Class notes & Summaries
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Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
- Exam (elaborations) • 648 pages • 2024
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- $26.08
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Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
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Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
- Exam (elaborations) • 648 pages • 2024
-
- $23.94
- + learn more
Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
-
Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
- Exam (elaborations) • 648 pages • 2024
-
- $22.69
- + learn more
Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
-
Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
- Exam (elaborations) • 648 pages • 2024
-
- $27.45
- + learn more
Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
-
Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
- Exam (elaborations) • 647 pages • 2024
-
- $29.14
- + learn more
Solution Manual for Rocket Propulsion, 1st Edition by Stephen D. Heister, 9781108422277, Covering Chapters 1-13 | Includes Rationales
-
Solution Manual: Rocket Propulsion 1st Edition by Stephen D. Heister - Ch. 1-13, 9781108422277, with Rationales
- Exam (elaborations) • 647 pages • 2024
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- $30.49
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Solution Manual: Rocket Propulsion 1st Edition by Stephen D. Heister - Ch. 1-13, 9781108422277, with Rationales
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Rocket propulsion, Self assesments|2023 LATEST UPDATE|GUARANTEED SUCCESS
- Exam (elaborations) • 4 pages • 2023
- Available in package deal
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What is the reason for multi-staging compared to single stage rockets? 
1. Higher payload ratio for same velocity increment 
2. Higher attainable velocity for same payload ratio 
 
 
 
Which forces need to be taken into account to calculate a launch vehicles trajectory at lift-off? 
1. Atmospheric drag force 
2. Gravitational force 
3. Thrust Force 
 
 
 
Why is the Hohmann transfer orbit considered most fuel efficient to go from Earth orbit to Mars orbit? 
Velocity increments are collinear to o...
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Rocket Propulsion Elements 12|2023 LATEST UPDATE|GUARANTEED SUCCESS
- Exam (elaborations) • 3 pages • 2023
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in SRMs, the propellant is contained and stored 
directly in the combustion chamber 
 
 
 
grain 
-solid body of the hardened propellant 
-accounts for 82 to 94% of total motor mass 
-burns on its exposed inner surfaces 
 
 
 
igniter 
-provides the energy to start combustion 
-electrically activated 
 
 
 
nozzle 
-accelerates the hot gas 
-made of high temp materials 
-hot reaction gases flow along perforation or port cavity toward nozzle 
 
 
 
because there is no active cooling... 
the motor...
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rocket propulsion final|2023 LATEST UPDATE|GUARANTEED SUCCESS
- Exam (elaborations) • 2 pages • 2023
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What are advantages of an end burning charge? 
Highest value of loading fraction 
 
 
 
What are the main component of solid rocket motors? 
Ignitor, casing and insulation, solid propellant grain, nozzle 
 
 
 
What are solid rocket propellant's classes? 
colloidal, composite, and CMDB 
 
 
 
What are properties of colloidal propellants? 
unstable, homogenous, can combust without other materials 
 
 
 
What are properties of composite propellants? 
stable, higher performance, better burn rate c...
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Rocket Propulsion (1)|2023 LATEST UPDATE|GUARANTEED SUCCESS
- Exam (elaborations) • 2 pages • 2023
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- $11.49
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1. Which of Newton's Laws describes how a rocket works? 
Action - Reaction: Newton's Third Law 
 
 
 
2. Explain the difference between Thermodynamic and Electrodynamic propulsion systems used on spacecraft 
--Thermodynamic (heat/pressure energy) 
i. Cold gas 
ii. Liquid chemical 
Monopropellant 
Bipropellant 
iii. Solid chemical 
iv. Hybrid chemical 
v. Nuclear thermal 
vi. Arc-jet 
vii. Resisto-jet 
viii. 
--Electrodynamic (electromagnetic energy) 
i. Ion thruster 
ii. Plasma rocket 
 
 
 
3...