How Far Can My Model Rocket Reach in Space?

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The discussion centers on a model rocket designed to track light using sensors and an Arduino microcontroller, intended to launch from a balloon when it pops. While the rocket could potentially reach several thousand feet, the control system may fail at high altitudes due to insufficient air for the fins to function effectively. Experts suggest that vectored thrust could provide better control in low-pressure conditions. Additionally, the extreme cold in the upper atmosphere could freeze electronics and make structural components brittle, risking the rocket's integrity. Overall, reaching space presents significant challenges beyond just altitude.
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I've built a model rocket with the longest burning engine I could find, a light sensor in the nose cone, accelerometers on the forward fins all connected to an Arduino pro mini microcontroller programmed to keep it pointed at the brightest source of light. If I attach this rocket to a balloon and set it so that the microcontroller fires the engine when the balloon dramatically loses pressure (it pops), and assuming everything goes right - the rocket expends most of its fuel while pointing at the sun/moon when they are at the highest point in the sky... How far could my rocket get? Can it survive the conditions of space?

Yes I know building a guided rocket that chases the brightest light it sees is probably frowned upon in some places, I doubt it'll be a problem where I live.
 
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Welcome to PF. Based on the tone of the question, I'd say you'll get a few thousand feet above the balloon. Your biggest problem will be that your control system won't work at high altitude - there isn't enough air for the fins to grab.

Getting into space is not as easy as you think.
 
I'm no expert on space but I would think that controlling the rocket's direction through vectored thrust rather than movable fins would result in better control in a low pressure atmosphere.

But perhaps you should clarify what you mean by "space". The Earth's atmosphere has several regions and actual "space" doesn't begin for several hundred miles.

My opinion is that if you should manage to make it to the outer edge of the atmosphere the extreme cold will freeze the electronics (causing them to malfunction or stop altogether) and some important stuctural components. Certain materials such as some plastics and even certain grades of common metals become very brittle at extreme low temperatures and the vibration from the engine could shatter the rocket.
 
Venus does not have a magnetosphere, so the Galactic Cosmic Rays (GCRs) environment shall be much worse than in a LEO environment. Looking to the std radiation models for Venus, the standard radiation-hard space level electronic component with tested immunity LET = 85 MeV-cm2/mg seems not enough, so, for example, a 1cm2 Si die will suffer considerable flux above this level during a long mission (10 years for example). So, the question is, usually we are not paying attention to latch-up...
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
Thread 'SpaceX Starship development: 7th flight January 10'
Watch the progress live This is a fully stacked Starship (top) and Super Heavy (bottom). A couple of too-small-to-see cars near the bottom for scale, I also added a Saturn V and the Statue of Liberty for comparison. 120 meters tall, about 5000 tonnes when fully fueled. Twice the mass and over twice the thrust of Saturn V. The largest rocket ever built by mass, thrust, height, and payload capacity. N1 had the largest diameter.[/size] But its size is not the revolutionary part. It is designed...

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