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2022-05-04 LAB Meeting notes
Date
May 4, 2022
Attendees
@James May (RIT Student)
@Brahm Soltes (RIT Student)
@Kenny Kim (RIT Student)
@Paige Elias (RIT Student)
@Wynter Brigitta-Maita (RIT Alumni)
@Domenic Cacace (RIT Student)
@Grace Dertinger (RIT Alumni)
Goals
Get actionable steps to get trainings, testing, & lab access
Simulations/Calculations
High-level Full Rocket CFD to find max drag
Snatch Force verification
Shock Cord maximum snatch force
Component verification
Bulkheads FEA
Nose cone CFD
Fin FEA/CFD
Free Body Diagrams of individual components during launch and recovery
Falling speeds to ensure there is no collision during recovery
Testing
Rocket epoxy connection (verification of assumed connection strength)
Metal to CF bond
CF to FG bond
Blue tube to FG
Blue tube to CF
Thermal expansion of interfaces and what the implications are
Heat energy generation from COTS solid motors
Find Material properties of layup airframe using tensile or compression testing
Recovery deployment charge testing
Discussion items
Time | Item | Who | Notes |
|---|---|---|---|
| Simulations/Calculations | Launch/LAB |
|
| Testing | Launch/LAB | Rocket epoxy connection (verification of assumed connection strength)
|
| Other Notes | Launch/LAB |
|
Roll Call
Launch
James May
Brahm Soltes
Domenic Cacace
Alex Speyer
Grace Dertinger
Paige Elias
Kenny Kim
LAB:
Mike Buffalin
Bob Carter
Wellin
Abbreviated Transcript
Confluence might be going away next year
Introductions of Launch members
Launch mission statement: "end goal of launch is to have a liquid rocket space shot"
Starting off with next steps and actionable items
Wellin: You are an official RIT club team, where is your funding coming from?
James: A little bit from the college, some cooperate sponsors via material and funding, crowdfunding
Wellin: Where are you housed?
James: Right now no home, the SHED will be the home once it's finished. We have been working in the Construct and store things in the basement
Wellin: Are all the teams competition related?
James: We have Space Race, IREC, propulsion R&D, avionics R&D
Wellin: Of the projects on the website, which ones are you working on? What is RL-36? VOID? FL-1? Ground station? Tuatara?
James: Liquid team is designing that and FL-1. VOID is the IREC rocket
Wellin: Is the solids team a thing?
Grace: We just got started and we're working with
Wellin: If you have any connection with Launch at all but you do things that are unsanctioned for, that's the fastest way to get cancelled. I don't want to want to be involved and be associated if I don't know what's going on. Liquids should not be no development, like no building and testing. You can't use equipment that RIT paid for.
Grace: There is no testing going on for liquid prop
Wellin: This is a condition for my involvement here. Everything must be proper
Grace: We want to learn and do everything the safest way possible, your concern is valid
Mike: Would it make sense for LAB to be strictly IREC?
Wellin: I don't know if this is more of an advisory or consultative role
Mike: Let's go over the discussion items so we can decide if it's more advisory or consultative
Wellin: What are the elements of the competition?
Brahm: There's a bunch of awards, there's a technical report, launch criteria, presentation.
Wellin: So it's a very cumulative score
Grace: Yep. So with your help, we need more knowledge
Wellin: What's the history of success?
Brahm: The first year we went, we got 11th, then in 2019 it exploded on the pad, then COVID, then 15th place with Blackout. The competition has grown a lot, the teams are a lot more competitive
Wellin: What are you trying to do to stay competitive?
Brahm: Last year, we did custom body tubes, custom payload, improving on avionics.
Wellin: Would SRAD or liquids be better?
Brahm: SRAD is a little less competitive. Liquids have a huge amount of expertise
Wellin: Why try to win in something that's easier? Why not focus all your efforts on the competition?
Grace: The other teams aren't diverting resources. We need your help with these technical things
Wellin: I know nothing about IREC. We can help looking through the report.
Mike: Are any of these development points for this year's report?
Grace: No, but it will help with next year.
Mike: A good start is testing rocket epoxy - is that even the best material to use?
James: We don't know. Can you help use do tensile test.
Wellin: I don't know how much material testing equipment we have left. MET might have some
Mike: There is a plastics lab
Mike: What CFD are you doing?
Brahm: Simscale, Ansys Fluent
Mike: What do you want with that CFD
Brahm: We've been doing it for small components to get drag, but we haven't done anything for the full rocket
Wellin: Are you doing compressible? Are you doing sub or supersonic? And you wrote you want to do wind tunnel testing?
Mike: The only wind tunnel on campus does like 90 mph? How much testing do some teams do?
Brahm: Some teams do nothing, especially if it's COTS. Others do a lot, including even vibration testing. Two years ago, there was a team that did a turbine.
James: What are our action items then?
Wellin and Carter: Taking a look at other technical reports will really help us.
Brahm: There's a good list of previous technical reports.
Mike: Definitely do the epoxy tensile tests
Wellin: Figure out what test you want to do and what kinds of standards you want to follow.
James: We'll do our research, you guys [LAB] reach out to the labs needed, and we'll meet in two-weeks time
Mike: Depending on the stresses in flight, 3-point bending might be good too
Wellin: You should talk to Formula, they do tests every year
James: I'll be here over the summer, we'll meet then.
Brahm: We want to also do deployment charge testing
James: We do these static tests for deployment charge testing, we would like to do it on campus but that gets complicated with black powder
Wellin: What are you doing for avionics testing? Is avionics being developed?
James: It's mostly COTS components
Brahm: Custom electronics are not allowed for deployment according the IREC rules
Mike: I'll work with EH&S and public safety about the black powder thing
James: For any single energetic device, it should be less than 5 grams of black powder
Grace: I'll send an email with what we discussed and the action items, but let's do one more action item
Brahm: I think the thermal expansion and loss in strength is important. Since we'll be in New Mexico, it will get really hot
Wellin: So the best case scenario is to hit exactly 10,000 ft?
Brahm: Yes, and you can only control roll, no other active controls
Grace: If you guys could look up more about IREC, that would be great
James: We should also prepare something for you to explain the parts of the rocket
Brahm: Circling back, on thermal tests, we thought about even putting the rocket in an oven
Grace: So we need to tell them what items exactly we want to do that heat tests for
Mike: The plastics lab has an oven with a tensile tester in it
Carter: What size of oven do you need?
James: Minimum is probably a 7-inch tube
Brahm: One thing we could do is firing a COTS motor and looking at the heat coming off of the casing
James: That's a Scott Williams thing, not tot relevant now. But we do want to test if the couple tube fit is affected by heat expansion
Carter: There's also heat testing you can do with the electronics and batteries.
Wellin: And the composites can be tested for heat
James: Is another meeting in 2 weeks time good?
Carter & Wellin: Yeah that should be good for us.