|
Rockets Down Under |
GDT-2 Mk1 Payload |
|
David Boyd's Australian Rocketry Home Page |
Overview of the GDT-2 Mk1 Payload |
| Features of the GDT-2 Mk1 payload was constructed to fly on the GDT2 flight. However shipping problems meant that it wouldn't
arrive in time. An alternative Payload was flown on GDT-2 using my new 75mm payload bus
system.. Described below is the Mk1 payload, which still has not flown. The features of the GDT-2 Mk1 payload are:
|
|
It has to start somewhere ! This is the electronics test bench in my workshop. |
|
This image shows most of the GDT-2 payload (upside down). Uppermost is the flight computer. Below left the backup timer, below right the backup battery, and below centre the on/off switches. The ribboncable on the left is the umbilical cable with connector. In front of this cable is the camera leed. |
|
Close-up view of the ALT5 flight computer. Click on the image to enlarge
it for a more detailed view. The largest chip is the microprocessor, with modem chip below it. The round silver disk is the altimeter pressure sensor. The accelerometer is located under the PCB. The four mounting holes are for a Motorola Oncore M12 GPS unit. |
|
The other side of the payload (upside down). From Top to bottom is the
transmitter antenna, ATV12-440 video transmitte (in shielded case), and 12V 2000mAh Ni-Cad
battery pack. Hidden in each of the bulkheads are the pyro charge cannisters and connectors. |
|
This is the ATV440 video transmitter with the shielded case removed. The aluminium bracket attaches to a large aluminium heatsink (not shown). |
This page created 17th July 2001, last updated 26th May 2002.
This page has been accessed times since 17th July 2001.
Return to... |
David Boyd's Australian Rocketry Home Page |