projects:storm
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Table of Contents
STORM
Stratospheric Observations and Radiation Monitoring
comments welcome: mrongen@halifax.rwth-aachen.de
Summary
- Still under development (T.B.D. = “to be done” or “to be determined”), no flight experience yet,…
- 4 AA Batteries, Latex Balloon
- 434.xxx Mhz, Shift xxx, xxx Baud
- Transmission every 30 second
Payload
- Five main modules clustered around central battery pack
- (mainly) I2C as communication protocol between modules
(System overview image)
Power Distribution Board (PDB)
- Distributes 6V from 4 AA batteries to all modules
- Mounted to back of standart battery pack
- Monitors battery voltage and total current via INA219 IC and 200mOhm shunt resistor
- Datasheet: http://www.ti.com/lit/ds/symlink/ina219.pdf
- Design Files: (Link)
Batteries
- Energizer Ultimate Lithium
- Datasheet: http://data.energizer.com/PDFs/l91.pdf
Flight Controle Unit (FCU)
MicroController and GPS
- NavSpark Microcontroller (originalle an Indigogo Campaign)
- 100MHz 32bit LEON3 Sparc-V8
- Full GPS support with external battery
- 2x UART, 2x SPI, 1x I2C, ~80uA/MHz @ 3.3V
- P1PPS time reference with ± 10nsec accuracy
- Software: (Link)
(Photo)
Inertial measurement unit (IMU) and Telemetrie Module
- Integrated buck-converter power supply to 3.3V for itself and the uC
- Design Files: (Link)
IMU
- BMP180: Temperature, Pressure and humidity sensor
- LSM303D: 3 axis accelerometer und magnetometer
- L3GD20: 3 axis gyrometer
Telemetrie
- Radiometrix NTX2
- T.B.D.: Quarter wave antenna with solid or wire ground
Storage
- not all data can be transmitted, but everything is stored for offline analyses
- 1 GB micro SD-Card interfaced via SPI
(Photo)
Sensor Fusion Board (SFB)
- distributes I2C to OTP, RD and PDB modules
- UART to GSM module
- +3V3 to OTP and PDB
- Design files: (Link)
Data packet structure and integration into the HabHub
T.B.D.
Outside Temperature Probe (OTP)
- BMP85 on breakout board
GSM-Module
- ElecFreak GSM Module
- Datasheet: (Link)
- integrated LDO power supply
- only powered up after landing, so to conserve battery and as the RD is EMI sensitive
- sends SMS with position, altitude, speed (hopefully zero) every X minutes
Radiation detector (RD)
Theory
Options
- PMT (Photomultipler) with Scintillator:
- + high sensitivity
- + good energy resolution
- - high voltage needed (~ 1kV)
- - heavy
- - suscaptible to temperature and magnetic field changes
- - complex to setup
- SIPM (Silicon photomultiplier) with Scintillator
- + high sensitivity
- + good energy resolution
- + lightweight
- - high voltage needed (~80V)
- - VERY sucaptible to temperature changes
- - complex to setup
- Geiger Müller tube
- + easy to setup
- + lightweight
- o average sensitivity
- - high voltage needed (~500V)
- - no energy information at all
- Solid state detector (Teviso RD3024)
- + trivial to setup
- + low voltage (~5V)
- + “some” energy resolution through the pulse with
- + lightweight
- - low sensitivity
- - EMI sensitive
Teviso RD3024 Module
- array of radiation soft PIN diodes
- integrated bias-, amplification-, comperator-, and output-shaping circuit
- ~6CPM/uSh/h, essentially stable from 3 - 6 V, -40 - 60 °C
- pulse width is supposed to be slightly correlated to particle energy (to be tested further)
- SMD package
- Teviso sponsored one unit, otherwise ~120€
Breadboard test
- ATTiny85 triggers on rising and falling edges of RD3024 TTL pulse
- pulse width resolution: 1us
- accuracy test with 130 us function generator pulses: 130.2 +- 2.3 us digitised
- ATTiny acts as I2C slave against FCU
(Photo and plots)
Flight module
- Integrates buck-converter power supply to 3.3V
- allows soldering a grounded aluminium EMI shield over the RD3024
- Design Files: (Link)
Camera
- FlyCamOne Eco V2 (Link)
- integrated power supply
- Video, Timed Pictures
- 720 x 480px @ 30 fps
- max. 8 GB Micro SD card
- 4-6 V input
Conformal coating
- breakdown voltage of air is drastically reduced at low pressures (Paschen Law)
- can lead to elevated discharge rates even at voltages below sparking
- coat PCBs and plugged connectors with Plastik70
Environmental testing
Vaccum
- T.B.D.: Test full electronics system with conformal coating for elevated discharge at Paschen minimum.
Temperature
- T.B.D.: Battery temperature is not supposed to drop below -10°C when exposing powered payload to -50°C for 20 minutes
EMI
- T.B.D.: Test GPS reception and RD noise during 70cm and GSM transmissions
Telemetries range
- Possibly a test chasing a commercial hot air ballon with the payload
Boyancy
- Should stay afloat on standing water for at least 10 minutes
Mechanical integration and isolation
T.B.D.
Ballon and Parachute
T.B.D.
Radar reflector
T.B.D.
Chase car
- Diamond MR-77S Mag Antenna
- Custom QFH antenna - T.B.D.
- FunCube Dongle (Link)
- DVB-T Dongle (Link)
Red Tape
- in Germany I need a Flugverkehrskontrollfreigabe (liftoff permission) from the Deutsche Flugsicherung (German airspace control)
- 2 weeks lead time
- this includes the need for a 1 day aviation insurance (~60€)
projects/storm.1420201571.txt.gz · Last modified: 2015/01/02 12:26 by storm