P3-D Spacecraft: Module Placement

These pages are under construction. If you have problems, corrections or suggestions - please let me know: DL1FDT

Module Position

Here is a overview of the modules integrated into the P3-D satellite, sortet by their place in one of the six equipment bays:

Side 1
- Liquid Ignition Unit (LIU)
- Cosmic-Ray Energy Deposition Experiment (CEDEX)
- Propellant Flow Assembly (PFA)
- Battery Charge Regulator (BCR) #3
Side 2
- A & B Cameras
- 2nd L Band Receiver
- 10m Transmitter, Digital
- S2 Receiver & HF Receiver
- 10m Transmitter, RF Output
- S1 Receiver & C Receiver
Side 3
Side 4
- K Band Transmitter & Ant.
- Array Release Unit (ARU)
- K Band Transmitter Osc.
- IF Matrix, LEILA, #2 C/D
- Power Supply Unit (PSU)
- Electronic Propulsion Unit (EPU)
Side 5
- X Band Transmitter TWTA
- RF Monitor Experiment
- X Band Transmitter
- Battery Charge Regulator (BCR) #2
- Global Positioning Satellite System (GPS) Experiment
Side 6
- Battery Charge Regulator (BCR) #1
- Sensor Electronics Unit (SEU)
- RUDAK-U
- L Band Receiver
- Internal Housekeeping Unit (IHU), Command Decoder
- Input/Output Module (I/O)
Miscellaneous
- The people working on the project.
- Sun Sensor
- Earth Sensor
- Reaction Wheels
- Umbilical Units
- CAN LAN
- Check-Out Terminal Equipment (COTE)
- SmartNodes
- Memory Modules (RAM)
- Spacecraft Antennas
- What the Orbit will look like.
- The Ariane launcher
- Propulsion Systems
- The 400N Thruster
- ARcjet Thruster (ATOS)
- Mechanical and Thermal Design

Last updated: Mar 4, 1996
Questions? Comments? Send mail to: Ralf Zimmermann