Initial Questions
Version 8 (J. Simmons, 05/25/2015 12:41 pm) → Version 9/12 (Aaron Harper, 05/25/2015 12:46 pm)
h1. Yavin Thruster Initial Questions v0.1
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h2. Project Background Questions
h3. BQ1. Why are we making this?
*BA1*. To create an educational project which combines both propulsion design and testing. In combination with the Shepard Test Stand technology yields a full turnkey package.
h3. BQ2. Who is this for?
*BA2.* Undergraduate aerospace and high level high school students and Mach30 Volunteers.
h3. BQ3. How will this be used?
*BA3*. Demonstrate fundamentals of propulsion systems design and testing of a cold gas thruster to include thrust, specific impulse, expansion ratio, chamber pressure, throat area, and controls.
h3. BQ4. Who's going to build this?
*BA4.* Mach30 volunteers,undergraduate aerospace and high level high school students with instructor involvement. Unit will be able to be built with commonly available components and 3D printed parts.
h2. Technical Requirement Questions
h3. TQ1a. What features does it need to have (now)?
*TA1a.* _The project needs to:_
* The thruster components from expansion chamber to nozzle are modular to allow experimentation and projects to be tested using the same hardware and parameters.
* Includes a set of sample CAD models for modification (templates)
* Gas flow must include a tank of fixed volume, pressure gauge, electrically actuated valve, and timing circuit to make comparison of designs possible.
* Must be operable indoors
* Control system must be integrated with test stand controls to synchronize operation with testing.
* Adaptable to Shepard Test Stand with minimum modifications (ideally just swapping the motor mount at first)
h3. TQ1b. What features does it need to have (later)?
*TA1b.* _In the future, the project (or related projects) may need to:_
* Variable gas flow for throttling
* Variable time valve operation for pulse width modulation and flow characteristics.
* Demonstrate ideal expansion, under- and overexpansion characteristics. This may require flow visualization capability (schlieren and/or CO2 vapor)
h3. TQ2. What are the legacy requirements?
*TA2.* _To maintain compatibility with other projects, the system should:_
* _..._
h2. Project Requirement Questions
h3. PQ1. How many do we want to make?
*PA1.* _..._
h3. PQ2. What is the budget?
*PA2.* _..._
h3. PQ3. What is the timeline?
*PA3.* _..._
h3. PQ4. What waste products will be produced by the manufacture and/or operation of this?
*PA4.* _..._
{{toc}}
h2. Project Background Questions
h3. BQ1. Why are we making this?
*BA1*. To create an educational project which combines both propulsion design and testing. In combination with the Shepard Test Stand technology yields a full turnkey package.
h3. BQ2. Who is this for?
*BA2.* Undergraduate aerospace and high level high school students and Mach30 Volunteers.
h3. BQ3. How will this be used?
*BA3*. Demonstrate fundamentals of propulsion systems design and testing of a cold gas thruster to include thrust, specific impulse, expansion ratio, chamber pressure, throat area, and controls.
h3. BQ4. Who's going to build this?
*BA4.* Mach30 volunteers,undergraduate aerospace and high level high school students with instructor involvement. Unit will be able to be built with commonly available components and 3D printed parts.
h2. Technical Requirement Questions
h3. TQ1a. What features does it need to have (now)?
*TA1a.* _The project needs to:_
* The thruster components from expansion chamber to nozzle are modular to allow experimentation and projects to be tested using the same hardware and parameters.
* Includes a set of sample CAD models for modification (templates)
* Gas flow must include a tank of fixed volume, pressure gauge, electrically actuated valve, and timing circuit to make comparison of designs possible.
* Must be operable indoors
* Control system must be integrated with test stand controls to synchronize operation with testing.
* Adaptable to Shepard Test Stand with minimum modifications (ideally just swapping the motor mount at first)
h3. TQ1b. What features does it need to have (later)?
*TA1b.* _In the future, the project (or related projects) may need to:_
* Variable gas flow for throttling
* Variable time valve operation for pulse width modulation and flow characteristics.
* Demonstrate ideal expansion, under- and overexpansion characteristics. This may require flow visualization capability (schlieren and/or CO2 vapor)
h3. TQ2. What are the legacy requirements?
*TA2.* _To maintain compatibility with other projects, the system should:_
* _..._
h2. Project Requirement Questions
h3. PQ1. How many do we want to make?
*PA1.* _..._
h3. PQ2. What is the budget?
*PA2.* _..._
h3. PQ3. What is the timeline?
*PA3.* _..._
h3. PQ4. What waste products will be produced by the manufacture and/or operation of this?
*PA4.* _..._