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STING: Simultaneous Thermodynamic and Inflow Networking via radiosonde Groups

STING: radiosonde balloons fanned out across a supercell

STING, short for Simultaneous Thermodynamic and Inflow Networking via radiosonde Groups, is the radiosonde system we design and build. A full sonde costs about $43 in parts, which makes it practical to launch several at once from different vehicles.

30+
Launches so far
3
Same-balloon reference flights
7
Sondes per radio channel
87 mi
Farthest tracking
Summary

STING at a glance

Measurements: temperature, humidity and pressure, plus GPS position for winds. Up to seven sondes share one radio channel. Receivers in our vehicles upload the data, and each flight appears live in the Recon Weather app.

Validation: three same-balloon co-flights with a NIST-traceable InterMet iMet-4, and comparisons with Vaisala RS41 radiosondes.

Field use: 30+ launches, a five-sonde launch, reception to about 140 km, a near-storm inflow sounding and a flight through a hail core.

Background

Radiosonde basics

A radiosonde is a balloon-borne instrument package that transmits pressure, temperature, humidity and GPS position during ascent, producing an in-situ vertical profile of the troposphere and lower stratosphere.

Measurements

TemperatureVertical temperature profile and lapse rates. Steep low- and mid-level lapse rates indicate potential instability.
Humidity & dew pointMoisture by layer, dew point depression and LCL height. Low-level moisture sets the energy available to convection.
PressureThe vertical coordinate for each observation, used to derive geopotential height.
Wind speed & directionDerived from GPS drift. The hodograph gives vertical wind shear and storm-relative helicity, key ingredients for supercells.

Applications

In-situ reference

Direct measurements that radar retrievals, satellite soundings and model analyses are compared against.

Model initialization

Operational soundings, launched twice daily worldwide, are assimilated into numerical weather prediction models.

Convective parameters

CAPE, CIN, bulk shear, helicity and LCL height from a single profile characterize the convective environment.

Design

System design

The sonde transmits raw readings. Processing, quality control and archiving are done on our servers.

01

The sensors

A small thermistor measures air temperature, a digital sensor measures humidity, and a barometer measures pressure, with GPS-derived pressure taking over high in the atmosphere. GPS tracks position, and winds are worked out from the drift.

  • Temperature
  • Humidity
  • Pressure
  • GPS winds
02

GPS-timed slots

Up to seven sondes share one radio channel, each sending in its own GPS-timed slot. A sonde sends every 7 seconds, or every 2 seconds in fast mode. Receivers store what they hear and upload it to our servers.

  • 7 sondes per channel
  • TDMA
  • 7 s or 2 s fast mode
  • Store and upload
03

Two versions

The full sonde measures temperature, humidity, pressure and wind. The GPS-only version is the same platform with the weather sensors left off, built for winds in the lowest 6 to 9 km. Two full sondes plus four GPS-only units still give six wind profiles.

  • Full sonde
  • GPS-only (2027)
  • Mixed fleets
04

Low impact

Natural latex balloons and cotton line. Small balloons of 20 to 50 grams keep helium use and cost per flight down, so we can launch more often.

  • Natural latex
  • Cotton line
  • Less helium

Specifications

The production configuration as documented in our methods manuscript. Encoded resolution is listed where relevant; it is not the same as instrument accuracy.

Airborne unit

Controller
ESP32 with radio transmitter
GNSS
L76-series GPS module
Temperature
NTC bead thermistor, ratiometric 16-bit ADC, Steinhart–Hart fit to reference
Humidity
Capacitive polymer sensor with heater, span-corrected
Pressure
Barometric sensor at ≥ 400 hPa; hypsometric GPS-derived above
Enclosure
3D-printed, biodegradable
Power
Two lithium-primary cells in series (full); single LiPo (GPS-only)

Radio link

Band
900 MHz ISM band, TDMA
Modulation
Digital, 125 kHz bandwidth
TX power
22 dBm configured
Packet
32-byte binary snapshot, CRC-checked
Longest track
~140 km (87 mi), standard ground antenna

Timing

Scheduler
GPS PPS-disciplined, 1 s slots
Normal slots
7 per channel, 7 s cycle
Fast mode
2 s; 5 s above 6,706 m; 4 s below 3.6 V

Flight configurations

Default
20 g natural latex, 4 ft cotton line
Windy
30 g, 4 ft
High altitude
50 g, 6 ft
Maximum
150 g, 6 ft (reference co-flights)
Hardware cost
$43.14 full, $33.22 GPS-only (BOM estimate)
Per flight
$62.43 full, $44.93 GPS-only incl. balloon and helium

Data path

SondeSensors read at transmit time and packed into a 32-byte snapshot.
→
Radio downlinkOne-way 900 MHz broadcast in the sonde’s own GPS-timed slot.
→
Vehicle receiverDecodes, maps invalid fields to nulls, stores to flash.
→
UploadBatched store-and-forward over cellular or WiFi.
→
ServerCorrections, QC flags, GPS winds, derived indices, archive.
→
AppLive skew-T, track and parameters for everyone following.

Processing and quality control

Humidity correctionFitted on the August 5, 2026 same-balloon co-flight (R² = 0.98) and applied live as a derived field. The raw reading is always kept.
RHcorr = clamp(1.157 × RHraw − 2.28, 0, 100)
Pressure crossoverThe barometer is used within its rated range; above it, pressure is computed hypsometrically from GPS altitude. Every sample records which source it came from.
p ≥ 400 hPa → pressure sensor  ·  p < 400 hPa → GPS
Quality flagsReadings are flagged low-confidence where the humidity correction is extrapolated or the sensor lags in deep cold.
RHraw > 81%  or  T < −25 °C
Encoding resolutionWhat each field can represent in the packet, not how accurate the sensor is.
0.01 °C · 1 % RH · 0.1 hPa · 1 m · 0.05 V

Dew point is derived from the bead temperature and corrected humidity. Winds are derived on the server from the GPS track. Balloon ascent rate is not treated as a measurement of storm updrafts.

Calibration

Calibration and validation

On three flights in July and August 2026, a STING sonde and a NIST-traceable InterMet iMet-4 radiosonde flew on the same balloon, so both sampled the same column. Readings were matched by pressure level. STING has also been compared with Vaisala RS41 radiosondes.

● August 5, 2026 co-flight
Temperature
−0.98 °C mean, sd 0.55
From the surface to about 14 km. The calibration fitted on the first co-flight held unchanged on the next two.
Humidity
~5.7 % dry, raw
The raw sensor reads slightly dry at high humidity. A correction fitted on this flight (R² = 0.98) is applied live to our data.
Dew point
−0.60 °C corrected
Down from −1.68 °C before the humidity correction.
Highest flight
18,974 m reference apogee
A 150 g balloon carried the pair high. The STING battery browned out in deep cold at 14,755 m, and a heater is planned.

Source: our STING methods manuscript (draft v0.15, October 2026). Numbers are from individual flights and are reported as measured, not as guaranteed accuracy. The humidity correction was fitted on this same flight, so its fit describes calibration data rather than an independent check.

Field results

● September 1, 2026 · Nebraska

Launched on the inflow side of a supercell, ahead of the rain core, so the sonde sampled the undisturbed inflow environment.

Burst altitude
10,257 m
A full profile of the inflow environment.
Instability
~2,800–3,000 J/kg CAPE
A strongly unstable environment with a low cloud base, around 790 m.
Deep-layer shear
57–63 kt, 0–6 km
Strong shear. Low-level (0–1 km) shear was marginal.
Model check
0.07 °C mean temperature difference
Close match to an HRRR model analysis, with dew point within 1.2 °C. This shows consistency with the model, not instrument accuracy.
Into a hail core · August 20, 2026A sonde launched under a 60+ dBZ hail core kept transmitting through saturated layers and a fast, precipitation-loaded descent with no electrical failure.
Five at onceThe largest coordinated launch so far: five sondes from two sites about a mile apart, released roughly 90 seconds apart.
87 milesA sonde tracked to about 140 km on the standard ground antenna, still decoding when the flight ended.
All kinds of weatherFlights in fair weather, rain, high wind, high and low humidity, cold, heat, and supercell environments.

The CAPE and shear values are first-pass STING estimates pending a full parcel analysis.

2027

2027 plans

Build enough full and GPS-only sondes for coordinated launches from several vehicles across storm boundaries and around supercells. A methods paper describing the system is in progress.

◆ 2027 fundraiser

Support the 2027 field season

The 2027 budget includes 200 full STING radiosondes and 160 GPS-only sondes, plus helium and field equipment.

$25,000
Proposed 2027 fundraiser goal
Current partial estimate: $22,305