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Voo 3032

Flight 3032

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
197.45m
6.47 s after launch
Máx. subida
67.87m/s
peak ascent
Máx. durante combustão
11.93G
during the burn
Aterragem
27.14s
touchdown 8.48 m/s
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Resumo do voo

The flight, moment by moment

Liftoff
0 s
Inclinação rampa32.77°
Thrust calc pad tilt4.6°
Launch detected
0.845 s
Altitude30.05 m
Velocidade65 m/s
Fim combustão (primeiro)
1.11 s
Altitude47.91 m
Velocidade67.350 m/s
Apogeu
6.47 s
Altitude197.45 Metros
Incl. máx. até fim comb.11.01°
Possível ejeção
8.316 s
Altitude180.74 m
Velocidade-12.94 m/s
Aterragem
27.14 s
Altitude-2.4 m
Máx. descida-26.83 m/s

Estabilidade82.9%Bom

Inclinação no fim da queima (20%)88.3
20% · Launch tilt 4.6°
Taxa arfagem/guinada (30%)89.7
25% · Coning 33.7/56.4°/s
Coning · boost (25%)75.8
25% · Spin 882.6°/s
Retidão de empuxo (15%)79.6
30% · Thrust 95.7%

Rocket information

Calculated from the flight data alone
Boost acceleration60.7 m/s²
average over the burn · 6.2 g
Coast deceleration12.6 m/s²
average · gravity plus drag
Ballistic coefficient173 kg/m²
fitted to the 5.36 s coast
Apogee lost to tilt0.63 m
flown vertical ≈ 198 m · from the thrust-calculated tilt
Chute opening peak45.84 G
largest deceleration after ejection
Average descent rate9.72 m/s
ejection to landing · 18.82 s
Bateria & temperatura 78% → 75% · Temperatura início 23.38 → 25.6 °C · Lançamento após arranque 15m 27s

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
Apogeu197.45 Metros
Tempo até apogeu6.47 s
Altitude fim combustão47.91 m
Altitude vel. máx.42.32 m
Altitude ejeção180.74 m
Altitude aterragem-2.4 m
Altitude gravação-78.07 m
Velocidade
Máx. subida67.87 m/s
Máx. descida-26.83 m/s
No fim combustão67.350 m/s
Vel. descida-9.726 m/s
Vel. ejeção-12.94 m/s
Vel. aterragem-8.484 m/s
Aceleração
Máx. durante combustão11.93 G
Máx. subida11.93 G
Máx. descida45.84 G
Média subida0.55 G
Média combustão6.27 G
Tempos
Fim combustão (primeiro)1.11 s
Apogeu6.47 s
Possível ejeção8.316 s
Aterragem27.14 s
Ângulos
Inclinação rampa32.77°
Thrust calc pad tilt4.6°
Incl. máx. até fim comb.11.01°
Rolagem no lançamento30.28°
Arfagem no lançamento10.56°
Rotação máx. (comb.)1366.09 dps
Rotação média (comb.)904.72 dps
Staging
Stages detected1
Burnout (refined)1.215 s
Stage S1 burnout
flip1.093 s
drag1.217 s
sig1.246 s
Recovery
Single deploy
No dual deploy detected on this flight.
Geral
Data envio04/10/26-12:22:21
Amostras de dados8569
Tempo total gravação44.262 s
Média amostras/s193.5
Número de bloqueios0
Lançamento após arranque15m 27s
Eixo de referênciaX
Bateria & temperatura
Bateria início78%
Bateria fim75%
Temperatura início23.38°C
Temperatura fim25.6°C
Notas do utilizador
Sem notas
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Vídeo Youtube
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Imagens do voo 0
Sem imagens
Motores do voo
1st stage · 6s delay
1×B6-6EstesDetails
Burn time
0.86 s
Diameter
18.00 mm
Average thrust
5.03 N
Max thrust
12.14 N
Total weight
19.10 g
Propellant weight
5.60 g
Propellant type
black powder
Impulse4.33Ns
Max thrust12.1N
Burn time0.86s
Impulse classB
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Foguete associado
Nenhum foguete associado a este voo
Flight mass
Liftoff mass52.4gestimated
Mass at burnout46.8gestimated
No mass is set for this flight, so Motor thrust (N) uses a mass estimated from the measured burn and the motors’ rated impulse. Set the rocket’s mass for the measured impulse and specific impulse.
Motor thrust (N) is on the chart, under Acceleration.

Other flights on this motor

1 · highest first

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.

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.

No launch site has been set for this flight.

Animação dos dados

FLIGHT 3032

197.45 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
Revision 4
Nano V1
Este voo foi realizado num Nano V1.
The hardware
Versão hardwareRev 4
Versão software1.65
Última ligação04/10/26-12:22:21
Sensor pressãoBosch BMP 581
Acelerómetro32G 3-axis
Giroscópio2000 dgps 3-axis

Flights from this altimeter

No other flights yet. This will fill up as you fly.

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⚠ O giroscópio não foi calibrado
X0.000°
Y0.000°
Z0.000°
Acelerómetro⚠ O acelerómetro não foi calibrado
X0.000 mG
Y0.000 mG
Z0.000 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
3032.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
806 KB
LOG
3032.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
89 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.

Voo
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