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DaVinki 0 Flight 1

Nano V1 Rev 4 · firmware 1.63Secure logSecure logThe altimeter signed this log and it passed verification on upload, so the data is unchanged since the device wrote it.Signatures use Ed25519, which no current technology can forge.
Apogeo
279.72m
7.88 s after launch
Máx. ascenso
97.65m/s
peak ascent
Máx. durante combustión
28.01G
during the burn
Aterrizaje
0s
touchdown 0.03 m/s
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Resumen del vuelo

The flight, moment by moment

Liftoff
0 s
Ángulo de rampa5.3°
Desvío de rampa19.11°
Aterrizaje
0 s
Altitud-0.66 m
Máx. descenso-25.83 m/s
Launch detected
0.658 s
Altitud30.24 m
Velocidad91.72 m/s
Fin combustión (primero)
0.74 s
Altitud38.97 m
Velocidad96.670 m/s
Posible eyección
6.915 s
Altitud274.85 m
Velocidad12.06 m/s
Apogeo
7.87 s
Altitud279.72 Metros
Incl. máx. hasta fin comb.23.79°

Estabilidad69.1%Moderado

Inclinación al apagado (20%)86.6
20% · Rail angle 5.3°
Cabeceo/guiñada (30%)79.2
25% · Coning 51.2/114.6°/s
Coning · boost (25%)43.1
25% · Spin 321.6°/s
Rectitud de empuje (15%)70.7
30% · Thrust 93.7%

Rocket information

Calculated from the flight data alone
Boost acceleration130.6 m/s²
average over the burn · 13.3 g
Coast deceleration13.6 m/s²
average · gravity plus drag
Ballistic coefficient199 kg/m²
fitted to the 7.13 s coast
Apogee lost to tilt10.59 m
flown vertical ≈ 290.3 m · from the tilt at burnout
Chute opening peak21.57 G
largest deceleration after ejection
Batería & temperatura 80% → 75% · Temperatura inicio 32.35 → 36.68 °C · Lanzamiento tras encendido 20m 0s

About the stability score

Worked out from the flight log between liftoff and 80% of apogee. It is independent of the angle the altimeter was mounted at, so it measures the flight rather than the fitting.

Inclinación al apagado (20%)20%How close to vertical it left the rod.
Cabeceo/guiñada (30%)25%How much the nose swung off the rocket's own axis across the whole ascent.
Coning · boost (25%)25%The same swing during the burn, when it matters most.
Rectitud de empuje (15%)30%How cleanly the motor pushed along the body.

Spin about the rocket's own axis is not counted against it — a fast, straight spin is stable. The figures beside the score are the raw measurements behind these four.

Altitud
Apogeo279.72 Metros
Tiempo al apogeo7.87 s
Altitud fin combustión38.97 m
Altitud vel. máx.45.49 m
Altitud eyección274.85 m
Altitud aterrizaje-0.66 m
Altitud grabación-6.61 m
Velocidad
Máx. ascenso97.65 m/s
Máx. descenso-25.83 m/s
En fin combustión96.670 m/s
Vel. descenso-3.799 m/s
Vel. eyección12.06 m/s
Vel. aterrizaje0.034 m/s
Aceleración
Máx. durante combustión28.01 G
Máx. ascenso45.26 G
Máx. descenso21.57 G
Prom. ascenso1.64 G
Prom. combustión14.67 G
Tiempos
Fin combustión (primero)0.74 s
Apogeo7.87 s
Posible eyección6.915 s
Aterrizaje0 s
Ángulos
Ángulo de rampa ?5.3° ± 0.31°
Desvío de rampa ?19.1°
Incl. máx. hasta fin comb. ?23.79°
Orientación ?67.26°
Desalineación de montaje ?3°
Alabeo al lanzamiento-66.77°
Cabeceo al lanzamiento-10.85°
Giro máx. (comb.)1885.64 dps
Giro prom. (comb.)542.4 dps
Staging
Stages detected1
Burnout (refined)0.765 s
Stage S1 burnout
flip0.742 s
drag0.760 s
sig0.895 s
Recovery
Single deploy
No dual deploy detected on this flight.
General
Fecha subida06/09/26-19:23:31
Muestras de datos11889
Tiempo total grabación88.732 s
Prom. muestras/s133.9
Número de bloqueos0
Lanzamiento tras encendido20m 0s
Eje de referenciaX
Batería & temperatura
Batería inicio80%
Batería fin75%
Temperatura inicio32.35°C
Temperatura fin36.68°C
Something look wrong with this flight's data?
Tell us what looks wrong and we'll look into it. It helps us find and fix problems in the firmware and on the site, and we can correct this flight.
You're not logged in, so we can't let you know when we've looked into it.
Notas del usuario
Sin notas
Añada este dispositivo a su cuenta para editar
Vídeo Youtube
Sin vídeo
Añada este dispositivo a su cuenta para editar
Imágenes del vuelo 0
Sin imágenes
Flown as
Rocket
None
not linked
Motor configuration
Custom
1× Quest D16-8, set on this flight
Loaded weight
107.5 g
estimated, none entered

Measured burn

from this flight’s thrust
Total impulse, NFPA 1125needs the weight
rated 12.40 Ns
Burn time, NFPA 11250.75 s
0.01 to 0.76 s
Peak thrustneeds the weight
at 0.14 s
With no loaded weight the impulse would only give the motor’s rating back, so it waits for the weight. The burn time is measured either way.
Motores del vuelo
1st stage · 8s delay
1×D16-8QuestDetails
Burn time
0.79 s
Diameter
18.00 mm
Average thrust
15.6 N
Max thrust
22.3 N
Total weight
25.60 g
Propellant weight
12.50 g
Propellant type
Black Max
Impulse12.4Ns
Max thrust22.3N
Burn time0.79s
Impulse classD
1st stage thrustloading curve…
Motor data by ThrustCurve.org
Añada este dispositivo a su cuenta para editar
Cohete vinculado
Ningún cohete vinculado a este vuelo

Linked flights

Connect flights that belong together: a second altimeter flown in the same rocket, or the same rocket flown again. Linked flights appear on each other’s pages.

No linked flights yet.

Sitio de lanzamiento, fecha y hora

Haga clic en el mapa para marcar su sitio de lanzamiento. Cambie entre vista de mapa y satélite.

Imagery © Esri, Maxar, Earthstar Geographics

Clic en el mapa · Arrastre para ajustar

Canopy height from the Meta and WRI High Resolution Canopy Height Maps v2 (Meta and World Resources Institute, 2026; source imagery © 2016 Vantor), used under CC BY 4.0. Ground elevation built from Terrain Tiles (Mapzen and AWS Open Data), derived from 3DEP and GMTED courtesy of the U.S. Geological Survey, SRTM courtesy of NASA, and ETOPO1 courtesy of NOAA. Map and imagery credited on the view above.

Site nameUnnamed siteLat52.258201Lng-0.093819Ground level52.0 m · 170 ftFecha lanzamiento2026-09-06Hora lanzamiento—
Animación de datos

FLIGHT 2886

279.72 Meters

ALTITUDE
0.00m
VELOCITY
0.00m/s
ACCEL
0.00G
TILT
0.00°
PITCH
0.00°
ROLL
0.00°
YAW
0.00°
TIME
0.00s
AWAITING LAUNCH
ALT
altimetercloud.com
LAUNCH T+0.00s LANDING

BURNOUT

Motor burn complete

Nota: La animación de vuelo requiere que su altímetro esté montado en una orientación fija. Calibre sus sensores para mejores resultados.
Nano V1
Rocketry Ltd

Nano V1

Altímetro compacto para cohetes pequeños. Este vuelo se realizó con un Nano V1.
Versión hardware Rev 4Versión software 1.63Última conexión 06/09/26-19:23:31

Especificaciones

Electrónica

Microcontrolador
ESP32-S232-bit ESP32-S2 240MHz
Acelerómetro
ST LSM6DSO3232G 3-axis (SPI)
Barómetro
Bosch BMP581300 to 1250 hPa within specification
Giroscopio
ST LSM6DSO322000 dgps 3-axis

Registro de datos

Frecuencia de muestreo máxima
833 Hz
Máximo de muestras por registro
38,000
Registro más largo
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Electrónica

Microcontrolador
ESP32-S232-bit ESP32-S2 240MHz
Acelerómetro
ST LSM6DSO3232G 3-axis (I2C)
Barómetro
Bosch BMP581300 to 1250 hPa within specification
Giroscopio
ST LSM6DSO322000 dgps 3-axis

Registro de datos

Frecuencia de muestreo máxima
833 Hz
Máximo de muestras por registro
38,000
Registro más largo
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Tamaño, peso y batería

Tamaño
20 × 10 × 8.9 mm
Peso
1.65 g1.65 g con la batería más pequeña
Voltaje de la batería
3 a 4.2 V
Duración de la batería
5con la batería más pequeña
Tamaño
20 × 10 × 8.9 mm
Peso
1.65 g1.65 g con la batería más pequeña
Voltaje de la batería
3 a 4.2 V
Duración de la batería
5con la batería más pequeña

Documentos

Flights from this altimeter

2 of 220 of 117

Settings, as they were for this flight

Ajustes generales del vuelo
Presión prevista
i
Set this to your local forecast pressure at sea level. This will offer you slightly improved accuracty for your flight, although it's not 100% essential every little helps!

Xcweather.co.uk is a decent place to grab pressures from for your location and time.
1013.2 mbar
Detección lanzamiento
i
This is the altitude above the launch pad altitude where the altimeter will trigger itself into recording / flight mode.

The altimeter keeps a constant average of the pressure while waiting for launch, it uses a simple algorithm and the pre-flight buffers to do this. The most recent 120 samples (~4 seconds) are ignored so your pre-trigger altitude won't effect the ground baseline.

For almost all uses we suggest keeping this on the 25 Meter (~82 feet) default settings. If you want to test your altimeter by throwing it in the air, or are planning a very low flight you may want to lower the setting.
30 meters
Sample ratio
i
The altimeter runs at 50Hz however you can record every sample or every X samples in order to extend the log time. For example if you set the ratio to 1 it will save 1:1 samples, or if you set it to 3 it will save 1 in 3 samples.
1:1:1 (400Hz)
Max samples
i
This is the maximum samples the altimeter will log per flight. When it reaches this amount it will stop and save the recording.
38000
Recording stop
i
This setting is how the altimeter decides to stop recording. You can choose either 450 (~9s) or 900 (~18s) samples stable or it will record until the max samples limit unless you press the BUTTON in Manual stop mode.

The samples stable method waits for the devices altitude not to change for the set number of samples. This is defined by not changing by more than +/- 1.0 meters for 98% of the samples, it's a reliable method to stop the recording after landing within 8-10 seconds (300 sample) or 16-20 seconds (600 sample).
Auto: 8s stable altitude
Oversampling
i
Oversampling is a internal setting of the BMP 390 pressure sensor. It is how many samples are taken for each reading. By taking multiple samples for each pressure reading the altimeter reduces noise and increases the resolution of the output.

The sensor can run at 50 samples per second in 4X mode, so we suggest leaving it in this mode as it will offer the highest accuracy.
16x Oversampling
IIR filter
i
The IIR filter is another internal sensor for the BMP390 pressure sensor. It is a Infinite impulse response filter used to enhance pressure measurement accuracy by reducing noise. It's primarily for smoothing out rapid pressure changes.

We suggest not setting this too high as it will cause delay to changes in altitude if set very high.
COEFF 7
Pressure filter
i
This filter is a software Kalman filter that runs on the altimeters processor.

The Kalman filter uses a prediction step based on a system model and then a correction step using new measurements to refine its estimate, it creates accurate most certain results from data with noise in it.
TruePath
Sample speed
i
The sample rate of the altimeter's sensors. 50Hz takes 50 samples per second, 100Hz takes 100 samples per second for higher resolution data.
400 Hz
Hybrid mode
i
When enabled, the altimeter records at full speed during ascent then switches to half speed after apogee to extend recording time during descent.
Enabled
Sync sensors
i
The filters on the pressure sensor can cause it to lag very slightly behind the Accelerometer and Gyroscope data. The Sync sensors option detects how far out of sync these sensors are. It then corrects the Acceleration and Gyroscope readings to match the pressure sensor.
ACTIVADO (46 samples / 114.88ms)
Orientation
i
This is the orientation you intend to install the Altimeter in your rocket. It's needed to ensure completly accurate angles and orientation charts and reports. Check out the Manual for more information on this.
Down (text up)
IMU filter
i
The IMU filter, or fusion filter takes the data from each axis of the Gyroscope and Accelerometer to calculate the Pitch, Roll, Yaw and tilt angle from vertical. These filters can build up some discrepency over time so it's important to calibrate your sensors to minimise this.
Madgwick 6-Axis
Launch ALP
i
This is prevention against accidental launch detection.

With this disabled the launch is based only on pressure and something that creates a low pressure can trigger the flight by accident. For example pulling your nose cone off can even trigger it.

With this enabled the rocket also needs to have seen 8 samples (0.25 seconds) of acceleration above this setting in the last 3 seconds as well as the pressure drop to trigger. There is a backup trigger of 1.05 seconds of altitude being above the launch detect setting too.

There are very few situations where this option would cause issues, so we suggest leaving it on.
2.0G
Launch lock
i
When enabled, the altimeter locks out recording for a set period after power on to prevent false triggering during setup.
DISABLED
Static temperature
i
A fixed temperature value used for altitude calculation when the external temperature sensor is disabled or not connected.
15 °C
Calibración de sensores
Compensaciones de calibración usadas en este vuelo.
Giroscopio
X2.000°
Y-0.173°
Z0.831°
Acelerómetro
X0.005 mG
Y1.310 mG
Z6.980 mG

Files

Where the altimeter signs its log, the file carries that signature and a tick beside it. A tick means the data is unchanged since the device wrote it, which is what a record claim needs.
CSV
2886.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
1152 KB
LOG
2886.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
148 KB
WX
2886_weather.json.gz
The weather for 48 hours either side of the launch, within 15 km of the launch site: NOAA GFS every hour, at the surface and up to about 31 km, and the NOAA GEFS ensemble where this site holds it. JSON, gzip compressed. Weather data by Open-Meteo.com (CC BY 4.0) and NOAA. For 2026-09-06 12:00 local time at 52.2582, -0.0938.
1136 KB
Adjusted CSV2904 recalculated in your browser
The log recomputed for your own sea-level pressure and temperature. Columns: time, altitude as recorded and adjusted, raw altitude as recorded and adjusted, pressure.

This file is built here from the signed log, so it carries no signature of its own. Anyone verifying a claim should be sent to the flight page and build their own from the original.

Custom CSVbuilt in your browser
Pick any of the chart’s data sets, the worked-out ones included, and the part of the flight to cover. Values come in the units the chart is set to.
In the file
Time span

One row for every time any chosen data set has a sample. A data set with no sample at that time is left blank rather than filled in. Built from the chart’s data, so it carries no signature.

Neil 06-Sep-2026 a las 21:54
Darn - you've found me a new thing.
Working on that now - I think the issue's quite clear in the fusion (main altitude output).
It's been caused by the large port pressure issue at launch, but shouldn't have caused that silly blip on ascent.

Hope the flight went well though!
JA
Jack14-Oct-2026 a las 21:04
Thanks!