Harness document
Flight Preparation Panel
Connector for charging and and debugging will be placed on a sidepanel PCB together with the remove-before-flight pins.
1,2 (OBC_TX, OBC_RX) RS-232 Debug interface for OBC on pins
3,4 (CANH, CANL) CAN on pins
5,6 (GND, V+) Charging connector directly to battery on pins
7,8 (GND, V+) Solar panel connector on pins
Connector pin map: TBD
1 3 5 7
2 4 6 8
4 remove-before-flight jumpers:
Antenna safety pin
Remove before flight
Kill switch
Solar panel deployment safety pin
Stack Connector
Stack connector: 18 pin double-row PC-104 connector (2.54mm pitch)
1 - CANH
2 - OBC_TX
3 - CANL
4 - OBC_RX
5 - ADCS GND
6 - ADCS 5V
7 - ADCS GND
8 - ADCS 5V
9 - P/L GND
10 - P/L 5V
11 - P/L GND
12 - P/L 3V3
13 - OBC GND
14 - OBC 3V3
15 - COM GND
16 - COM 3V3
17 - COM GND
18 - COM 3V3
Footprint pin map relative to PCB:
Center of pin 1 placed at (x=2.352mm,y=-27.264mm) measured from the board outline.
NOTE: The Stack Connector in the library has center of component in the center of pin1, and therefore the coordinates above can be used directly as the component x,y coordinates. Remember to set the origin before placing the connector.
Please see the stack connector placement PCBDoc for precise placement of stack connector and stack connector PCB library for stack connector footprint: Stack connector placement PCBDoc
(0,0) Y, Sidepanel D .___ ________________________ __ |/ |___| |___| \ / O O \ |17..18 | |15..16 | |13..14 | |11..12 | | 9..10 | | 7..8 | | 5..6 | | 3..4 | | 1..2 | | | | | X | Sidepanel A | | | | | | | | | | | \ _O_ _O_ / \__| |________________________| |__/
-=ADCS=-
Connectors to side panels: TBD
-=Solar Panel Connectors=- One connector from each side to EPS board.
Wires are soldered to the solar panels and connected to EPS with a 2 pin connector TBD.
Antenna Connector
MMCX snap lock connector placed on radio or COM board.
Cable: 2 mm thick 50 Ohm coax connected to antenna panel with MMCX connector.