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Lil' Nuke F41W-8

Nano V1 Rev 4 · firmware 1.65Secure 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.
Apogeu
295.05m
8.27 s after launch
Máx. subida
86.73m/s
peak ascent
Máx. durante combustão
12.77G
during the burn
Aterragem
43.15s
touchdown 5.92 m/s
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Resumo do voo

The flight, moment by moment

Liftoff
0 s
Ângulo da rampa38.3°
Desvio da rampa1.51°
Launch detected
0.941 s
Altitude30.04 m
Velocidade74.23 m/s
Fim combustão (primeiro)
1.16 s
Altitude48.77 m
Velocidade86.340 m/s
Apogeu
8.27 s
Altitude295.05 Metros
Incl. máx. até fim comb.38.9°
Possível ejeção
9.665 s
Altitude287.91 m
Velocidade0.37 m/s
Aterragem
43.15 s
Altitude0.07 m
Máx. descida-18.96 m/s

Estabilidade35.8%Razoável

⚠ Low confidence — altimeter may have moved in flight
Inclinação no fim da queima (20%)4
20% · Rail angle 38.3°
Taxa arfagem/guinada (30%)21.8
25% · Coning 188.9/91.1°/s
Coning · boost (25%)54.6
25% · Spin 130.3°/s
Retidão de empuxo (15%)53
30% · Thrust 89.7%

Rocket information

Calculated from the flight data alone
Boost acceleration74.4 m/s²
average over the burn · 7.6 g
Coast deceleration12.1 m/s²
average · gravity plus drag
Ballistic coefficient286 kg/m²
fitted to the 7.11 s coast
Apogee lost to tilt3.57 m
flown vertical ≈ 298.6 m · from the tilt at burnout
Chute opening peak39.19 G
largest deceleration after ejection
Average descent rate8.59 m/s
ejection to landing · 33.48 s
Bateria & temperatura 71% → 64% · Temperatura início 25.78 → 26.9 °C · Lançamento após arranque 2m 56s

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.

Inclinação no fim da queima (20%)20%How close to vertical it left the rod.
Taxa arfagem/guinada (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.
Retidão de empuxo (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.

Altitude
Apogeu295.05 Metros
Tempo até apogeu8.27 s
Altitude fim combustão48.77 m
Altitude vel. máx.45.24 m
Altitude ejeção287.91 m
Altitude aterragem0.07 m
Altitude gravação-118.39 m
Velocidade
Máx. subida86.72 m/s
Máx. descida-18.96 m/s
No fim combustão86.340 m/s
Vel. descida-7.721 m/s
Vel. ejeção0.37 m/s
Vel. aterragem-5.925 m/s
Aceleração
Máx. durante combustão12.77 G
Máx. subida16.6 G
Máx. descida39.19 G
Média subida0.52 G
Média combustão7.63 G
Tempos
Fim combustão (primeiro)1.16 s
Apogeu8.27 s
Possível ejeção9.665 s
Aterragem43.15 s
Ângulos
Ângulo da rampa ?38.3° ± 0.49° pouco fiável, o suporte moveu-se
Desvio da rampa ?1.5° pouco fiável, o suporte moveu-se
Incl. máx. até fim comb. ?38.9°
Orientação ?87.71°
Desalinhamento de montagem ?101.9° a definição de orientação parece errada
Rolagem no lançamento87.37°
Arfagem no lançamento29.60°
Rotação máx. (comb.)1206.56 dps
Rotação média (comb.)149.21 dps
Recovery
Dual deploy detected
Drogue descent rate11.57 m/s
Main deploy altitude79.6 m
Main deploy time28.935 seconds
Main descent rate5.41 m/s
Geral
Data envio20/09/26-12:46:14
Amostras de dados10352
Tempo total gravação60.262 s
Média amostras/s171.7
Número de bloqueios0
Lançamento após arranque2m 56s
Eixo de referênciaZ
Bateria & temperatura
Bateria início71%
Bateria fim64%
Temperatura início25.78°C
Temperatura fim26.9°C
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Notas do utilizador

Lil' Nuke F41W-8 at FOG 20/09/26

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Vídeo Youtube
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Imagens do voo 0
Sem imagens
Flown as
Rocket
None
not linked
Motor configuration
None
no motor recorded
Loaded weight
None
not entered
Motores do voo
Nenhum motor adicionado a este voo
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Foguete associado
Nenhum foguete associado a este voo

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Local de lançamento, data e hora

Clique no mapa para marcar o local de lançamento. Alterne entre vista de mapa e satélite.

Imagery © Esri, Maxar, Earthstar Geographics

Clique no mapa · Arraste 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 nameFOGLat51.555799Lng-2.837371Ground level5.1 m · 17 ftData lançamento—Hora lançamento—
Animação dos dados

FLIGHT 2953

295.05 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: A animação de voo requer que o altímetro esteja montado numa orientação fixa. Calibre os sensores para melhores resultados.
Nano V1
Rocketry Ltd

Nano V1

Altímetro compacto para foguetes pequenos. Este voo foi realizado num Nano V1.
Versão hardware Rev 4Versão software 1.65Última ligação 20/09/26-12:46:14

Especificações

Eletrónica

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

Registo de dados

Taxa de amostragem máxima
833 Hz
Máximo de amostras por registo
38,000
Registo mais longo
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Eletrónica

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

Registo de dados

Taxa de amostragem máxima
833 Hz
Máximo de amostras por registo
38,000
Registo mais longo
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Tamanho, peso e bateria

Tamanho
20 × 10 × 8.9 mm
Peso
1.65 g1.65 g com a bateria mais pequena
Tensão da bateria
3 a 4.2 V
Autonomia da bateria
5com a bateria mais pequena
Tamanho
20 × 10 × 8.9 mm
Peso
1.65 g1.65 g com a bateria mais pequena
Tensão da bateria
3 a 4.2 V
Autonomia da bateria
5com a bateria mais pequena

Documentos

Flights from this altimeter

6 of 620 of 117

Settings, as they were for this flight

Definições gerais do voo
Pressão 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
Deteção lançamento
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.
ATIVADO (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
Calibração de sensores
Desvios de calibração utilizados neste voo.
Giroscópio
X-0.793°
Y0.368°
Z0.201°
Acelerómetro
X7.370 mG
Y-16.080 mG
Z-6.300 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
2953.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
983 KB
LOG
2953.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
119 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.

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