Project Horus High altitude balloon project

Horus 17

Technical information:

Launch date 16/10/2011, 10:14 am
Landing date 16/10/2011, 10:55 am
Flight duration 41 minutes
Launch site -35.1020, 138.8253
Landing site -34.9131, 139.2111
Flight path  Web, KMZ
Distance travelled 40.9 km
Maximum altitude 9,303 m
Average ascent rate 7 m/s
Impact speed 5 m/s
Flight computer MicroNut Flight Computer
GPS module uBlox 6 NEO-6Q + Sarantel GeoHelix antenna
Radio transmitter Radiometrix NTX2 25mw
Telemetry 300 baud RTTY, CRC16 checksum
Tracking Ground stations (distributed listener), 2 chase cars, web based tracker

Details:

Horus 17 was a test of a new 'Pico' payload - an extremely lightweight version of Mark's MicroNut design. Our lightest payload yet, it tipped the scales at just over 47 grams. In order to achieve such a light payload, sacrifices had to be made, with thermal insulation being virtually scrapped. It was hoped that this flight would highlight any issues we might encounter with the payload in future flights.

Preparation and launch:

Given the tiny payload & purpose of this launch (essentially a test), a small balloon was used which made for hassle free filling. The new MicroNut boards feature uBlox 6 GPS modules which acquire lock very quickly even from a cold boot - the payload took only seconds from being switched on to having acquired lock and transmitting valid telemetry.

With the short predicted flight duration, one car was sent ahead in advance before the balloon was launched. After about a 15 minute head start, the balloon was released in blustery conditions.

Flight & recovery:

Initially the flight appeared to be going as planned - a slightly higher than planned ascent rate of 7m/s would mean a reduced maximum altitude, but this was perfectly acceptable. However, after reaching only 9.3km the balloon burst - over 10km short of the anticipated 20km altitude. It's possible that the windy conditions and short payload tether used resulted in the payload swinging enough to hit the balloon & rupture it, ending the flight prematurely.

Fortunately we had a chasecar nearby at the time of burst & we were able to recover the payload with minimal difficulty - it landed in field beyond a ridge of hills, which made decoding it's exact position from the road difficult. The payload was retrieved by means of radio direction finding with a handheld yagi & receiver.

Despite the low altitude achieved, the flight was a success, proving the lightweight payload's capabilities. One of our regular team members wasn't able to make it for the day, but he was able to help out by decoding telemetry from home back in Adelaide (and following the chase on the largest tracker display we've used to date).

Joel's receive setup

Many thanks to those who helped out with tracking on the day, as well as VK5ZT, VK5ZD & VK5ACY for coming out & meeting us after the recovery. :-)