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Project: Rocket avionics - Class C    

Description


Lunar Numbat is an Australian and New Zealand space technology project, which is using commodity open-source hardware and software to build components that can be utilized as part of larger missions, including the White Label Space Google Lunar X-Prize team.  Several of the Lunar Numbat build team are members of the Connected Community HackerSpace, based in Melbourne.


The Lunar Numbat strategy is to start small and incrementally build-up in a step-wise fashion.  Along the way, delivering tried and tested, re-usable hardware and software components, such as AIko.


Even a small Class C rocket provides some engineering challenges, such as packaging (minimal size and weight) and telemetry (communications).


Jon's minimal Class C payload consists of ...

Several successful launches have been achieved and accelerometer data acquired.

(1) Class C rocket launch and (2) Arduino Mini with 3-axis accelerometer

Images Copyright (c) 2009 Marc Alexander and Jon Oxer


However, there were issues with the wireless communications, which will be resolved as part of the more sophisticated Class G rocket project.


A future exercise will be to retro-fit, back into the Class C rocket, some of the hardware and (more importantly) software components that are being developed for the Class G rocket launch.


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2 messages about this page
Oct 31 2009 by Luke Weston
f (received) = f (transmitted) * c / (c + rocket speed)

The transmitted frequency is ~ 433 MHz. Let's say that the rocket
velocity is, say, Mach 1, and c is the speed of light, ~ 3 * 10^8 m/s.
The speed of sound is approximately 300 m/s.

At a transmitter frequency of, say, 433 MHz, it's downshifted by only
Oct 31 2009 by maca_404
The issues you had with losing comm's with the cheap module do you
think this may have been because of a frequency shift caused by
doppler effect due to the rockets acceleration. ?
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