CU Spaceflight

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CU Spaceflight

CU Spaceflight

@cuspaceflight

A student society of undergraduates and PhD students at Cambridge University, pushing the limits of high altitude ballooning and rocketry.

Cambridge, UK 加入时间 Temmuz 2009
65 关注458 粉丝
CU Spaceflight
CU Spaceflight@cuspaceflight·
All of the parts of White Dwarf that have already been manufactured
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CU Spaceflight
CU Spaceflight@cuspaceflight·
White Dwarf’s injector, manufactured by Hubs, has undergone some final adjustments, and is now ready for assembly. Once the discharge chamber construction and lines cleaning is complete, we will be able to begin our Cold Flow testing, ahead of the first firings of White Dwarf.
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CU Spaceflight
CU Spaceflight@cuspaceflight·
Aquila - the second stage of our spaceshot attempt Griffin - is taking shape. Below are parts of the fin can, a bulkhead, and part of the assembled body
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CU Spaceflight
CU Spaceflight@cuspaceflight·
The White Dwarf team have put together a partial assembly of the cold-flow-testing apparatus. A cold-flow test is a test where water or fuel is injected into a mockup engine but not burnt, so that we can analyse the atomisation characteristics of the injector and its flowrates.
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CU Spaceflight
CU Spaceflight@cuspaceflight·
CUSF have had a hugely exciting 6 months finally getting back to in person meetings and manufacture. We welcomed a new committee at the AGM last week and are very excited for what’s to come!
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CU Spaceflight
CU Spaceflight@cuspaceflight·
@Erdayastronaut @CopSub Happy to share some of our results for both self-pressurising and COPV-pressurised vehicles! There's some fun and interesting subtleties that pop out of the analysis, it's definitely an interesting one. This is one particular performance map for our Griffin spaceshot rocket
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Everyday Astronaut
Everyday Astronaut@Erdayastronaut·
@CopSub I think I'm looking specifically for the PV/W chart of any given configuration. So I'm just trying to show that in a pressure fed system, there's a point where increasing pressure in the tank doesn't actually add overall performance to a rocket because of diminishing returns
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Everyday Astronaut
Everyday Astronaut@Erdayastronaut·
Anyone out there have a trade off chart between tank pressure and tank weight for COPVs? Maybe someone at @CopSub has dealt with this? I was making an estimate but I fear I can't just totally wing it like I had planned haha
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CU Spaceflight
CU Spaceflight@cuspaceflight·
Our Facebook is back up and running under our new committee after a long radio silence. Keep up to date with current projects and society events🚀 facebook.com/cuspaceflight/
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CU Spaceflight
CU Spaceflight@cuspaceflight·
CUSF have successfully completed the first static firing of our own hybrid rocket engine. A measured impulse of 53,855 Newton seconds means its the largest Nitrous Hybrid rocket ever fired in the UK. youtu.be/RYhfGLZWWco
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CU Spaceflight
CU Spaceflight@cuspaceflight·
With the firing of our new hybrid rocket engine only weeks away, the controlling electronics are starting to take shape!
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CU Spaceflight
CU Spaceflight@cuspaceflight·
Some photos of our latest project - a GPS disciplined oscillator for use with our radio systems. Massive thanks to @CamCircPCB for yet more great quality PCBs.
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CU Spaceflight
CU Spaceflight@cuspaceflight·
Yesterdays successful HAB launch to send three teddy bears into space for a local primary school. Thanks to @boconline for suppliying the helium for the launch!
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CU Spaceflight
CU Spaceflight@cuspaceflight·
@adacoghen leading to this eventual "successful recovery" (we were still getting GPS & telem from dart avionics)
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CU Spaceflight
CU Spaceflight@cuspaceflight·
@adacoghen Sadly the explosion broke the power switch on the lower avionics, so the dart separation mech never fired, and the whole lot stuck together
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