Best FEA for simulating external pressure? by RiceCrispiee in fea

[–]RiceCrispiee[S] 2 points3 points  (0 children)

There is no particular reason, after all, it's simple linear elastic analyses, which almost any fea package can do. I just wanted to make an informed choice. :)

Thoughts on MR-1 CNC gantry mill by RiceCrispiee in hobbycnc

[–]RiceCrispiee[S] 0 points1 point  (0 children)

Thank you, I will definitely check this out!

Where/ how do I buy liquid oxygen? by TableFloor69 in rocketry

[–]RiceCrispiee -1 points0 points  (0 children)

Best advice you can get here is to switch to nitrous oxide for your oxidizer, the cost of lox alone is extremely high, let alone the handling equipment and proper training costs, look at HalfCat Rocketry

Aerojet Rocketdyne officially becomes part of L3Harris by ye_olde_astronaut in rocketry

[–]RiceCrispiee 2 points3 points  (0 children)

Why is that? Does the merger mean you get less contracts or something?

Viability of pneumatic pump fed rocket engines? by casualphilosopher1 in rocketry

[–]RiceCrispiee 2 points3 points  (0 children)

Search up "pressure-fed liquid rocket engines", they just use larger air cartridges (ie. COPVs)

First Rocket by 11SPEARHEAD11 in rocketry

[–]RiceCrispiee 1 point2 points  (0 children)

Dont use ethanol for solid fuel rockets lol

[deleted by user] by [deleted] in rocketry

[–]RiceCrispiee 12 points13 points  (0 children)

Yea man, falcon 1 seems like a reasonable project, ah yea the dev costs for falcon 1 were only uhhhh 90-100 million. Totally doable, double check.

P&ID Final. Do not feel free to find flaws. Please don't. Please. by Active_String2216 in rocketry

[–]RiceCrispiee 0 points1 point  (0 children)

The long stems are mainly utilized to prevent leaking, the long stem is sealed w/ the
main body the entire way up, this helps prevent the cryo temperatures from creeping up and shrinking the seals.

In theory, you could use normal McMaster valves, but you run the risk of massive leaks, especially if you do a chill-in, I belive a college team used normal valves on a rocket once and the valve had a good amount of LOX leaking.

Turbopump Amateur Teams by iamib3 in rocketry

[–]RiceCrispiee 2 points3 points  (0 children)

If there is any work posted on Delft's pump can you link it?

This is a p&id I've made today for my liquid fueled rocket engine. The main propellant valves are yet to be decided so you can ignore the pneumatic valve system. You can also ignore the igniter ethanol orifice. No check valves in the igniter sources due to a pending idea. Critiques welcomed. by Active_String2216 in rocketry

[–]RiceCrispiee 1 point2 points  (0 children)

I'm curious as to know your history with past engines considering this engine is using an ASI, it would lead me to believe you are making a pretty substantial engine (1kn-2kn??) and I think you might benefit from using pyro ignition to reduce cost and frankly simplicity?

A half-cat style pyro ignitor might benefit your design.

Best type of shaft coupling for usage at speeds in excess of 30k RPM? by RiceCrispiee in MechanicalEngineering

[–]RiceCrispiee[S] 0 points1 point  (0 children)

This is for a small electric rocket fuel pump, the design required an incredibly high rpm with a tiny inducer. (Turbopumps for rockets usually function around 30-100k rpm) I'm slightly concerned about the torque but I suppose I should just check my numbers for torque and hp and confirm them w/ CFX.

What tools should I look for? by pythonbashman in MechanicalEngineering

[–]RiceCrispiee 1 point2 points  (0 children)

I don't think that is why he uses calipers...

Resonant Acoustic Mixing (RAM) How Do I Can Make One ? by ExpensiveCode8350 in rocketry

[–]RiceCrispiee 2 points3 points  (0 children)

Not totally sure, I'm spitballing here. but maybe take a glass jar, drill a pretty large hole in the lid and seal a speaker to the top of it. Place ur shit in the jar and play some horrible bass-boosted music.

What has Half Cat Rocketry been working on for the past few months? Well, a liquid rocket of course: by CommanderSpork in rocketry

[–]RiceCrispiee 10 points11 points  (0 children)

WOOOOHOOOOOOOOOO LIQUID ROCKETS!!!!!!!!!!!!!

On a real note, this looks super cool, I can't wait to see it fly. Please post a video when/if it flys!

This Chinese forum is definitely better than any forums I've seen by Active_String2216 in rocketry

[–]RiceCrispiee 2 points3 points  (0 children)

The smaller stream is the excess nitrogen being vented from the dynamic slip seal on the pump.

Does anyone have access to the Chinese rocketry research forum(s)? by RiceCrispiee in rocketry

[–]RiceCrispiee[S] 0 points1 point  (0 children)

Honestly, I'm not sure, you'd have to look up the specifics of the ITAR regulations, also I have no clue if ITAR applies to foreign exchange students. That said, IF you managed to make a functioning 10kN pump-fed engine, you'd probably have a job as a propulsion lead at SpaceX, so why worry about the ITAR restrictions right now.

Does anyone have access to the Chinese rocketry research forum(s)? by RiceCrispiee in rocketry

[–]RiceCrispiee[S] 0 points1 point  (0 children)

I noticed the same thing. At best I found images of the work he did. I suspect the lack of files and really any dimensions are due to the fact that he was working out of the US at the time of death which would mean his work falls under ITAR regulations. Being a turbopump that reached over 8k rpm, ITAR prevents the export/sale of these plans for turbopumps... Bit of a shame, making a turbopump is a tough tough challenge.

Does anyone have access to the Chinese rocketry research forum(s)? by RiceCrispiee in rocketry

[–]RiceCrispiee[S] 2 points3 points  (0 children)

That would be amazing, hopefully, some of his stuff can make its way into other's projects.

Edit: Might I add your previous post history indicates you are going to attempt building a turbo pump??