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Aphelion (2) flight 32

Nano V1 Rev 4 · firmware 2.00Secure 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
183.98m
6.28 s after launch
Máx. subida
72.69m/s
peak ascent
Máx. durante combustão
25.82G
during the burn
Aterragem
38.08s
touchdown 5.29 m/s
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Resumo do voo

The flight, moment by moment

Liftoff
0 s
Ângulo da rampa10.9°
Desvio da rampa5.48°
Fim combustão (primeiro)
0.38 s
Altitude0 m
Velocidade72.650 m/s
Launch detected
0.58109 s
Altitude30.11 m
Velocidade68.87 m/s
Possível ejeção
5.683 s
Altitude0 m
Velocidade m/s
Apogeu
6.28 s
Altitude183.98 Metros
Incl. máx. até fim comb.12.01°
Aterragem
38.07 s
Altitude0 m
Máx. descida-6.93 m/s

Estabilidade85.9%Excelente

Inclinação no fim da queima (20%)72.7
20% · Rail angle 10.9°
Taxa arfagem/guinada (30%)95.5
25% · Coning 21.5/48.6°/s
Coning · boost (25%)80.8
25% · Spin 518.7°/s
Retidão de empuxo (15%)90.8
30% · Thrust 98.1%

Rocket information

Calculated from the flight data alone
Boost acceleration191.2 m/s²
average over the burn · 19.5 g
Coast deceleration12.3 m/s²
average · gravity plus drag
Ballistic coefficient237 kg/m²
fitted to the 5.90 s coast
Apogee lost to tilt1.49 m
flown vertical ≈ 185.4 m · from the tilt at burnout
Chute opening peak35.33 G
largest deceleration after ejection
Bateria & temperatura 78% → 75% · Temperatura início 32.65 → 34.22 °C · Lançamento após arranque 4m 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
Apogeu183.98 Metros
Tempo até apogeu6.28 s
Altitude fim combustão0 m
Altitude vel. máx.17.14 m
Altitude ejeção0 m
Altitude aterragem0 m
Altitude gravação1331.07 m
Velocidade
Máx. subida72.68 m/s
Máx. descida-6.93 m/s
No fim combustão72.650 m/s
Vel. descida-5.625 m/s
Vel. ejeção m/s
Vel. aterragem-5.291 m/s
Aceleração
Máx. durante combustão25.82 G
Máx. subida51.89 G
Máx. descida35.33 G
Média subida1.65 G
Média combustão19.54 G
Tempos
Fim combustão (primeiro)0.38 s
Apogeu6.28 s
Possível ejeção5.683 s
Aterragem38.07 s
Ângulos
Ângulo da rampa ?10.9° ± 0.26°
Desvio da rampa ?5.5°
Incl. máx. até fim comb. ?12.01°
Orientação ?13.41°
Desalinhamento de montagem ?17.6°
Rolagem no lançamento13.14°
Arfagem no lançamento2.67°
Rotação máx. (comb.)741.97 dps
Rotação média (comb.)423.3 dps
Staging
Stages detected1
Burnout (refined)0.391 s
Stage S1 burnout
flip0.386 s
drag0.391 s
sig0.536 s
Recovery
Single deploy
No dual deploy detected on this flight.
Geral
Data envio23/10/26-21:09:53
Amostras de dados9248
Tempo total gravação51.369 s
Média amostras/s180
Número de bloqueios0
Lançamento após arranque4m 56s
Eixo de referênciaX
Bateria & temperatura
Bateria início78%
Bateria fim75%
Temperatura início32.65°C
Temperatura fim34.22°C
Notas do utilizador
Sem notas
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Vídeo Youtube
Sem vídeo
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Imagens do voo 0
Sem imagens
Flown as
Rocket
None
not linked
Motor configuration
Custom
1× Quest B14T-5, set on this flight
Loaded weight
63.2 g
estimated, none entered

Measured burn

from this flight’s thrust
Total impulse, NFPA 1125needs the weight
rated 4.97 Ns
Burn time, NFPA 11250.38 s
0.00 to 0.38 s
Peak thrustneeds the weight
at 0.09 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 do voo
1st stage · 5s delay
1×B14T-5QuestDetails
Burn time
0.38 s
Diameter
18.00 mm
Average thrust
13 N
Max thrust
17.65 N
Total weight
16.10 g
Propellant weight
2.30 g
Propellant type
Blue Thunder
Impulse4.97Ns
Max thrust17.6N
Burn time0.38s
Impulse classB
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Foguete associado
Nenhum foguete associado a este voo

Linked flights

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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 namePlayas Training Center - NSL WestLat31.943667Lng-108.548579Ground level1350.8 m · 4432 ftData lançamento2026-10-23Hora lançamento14:00
Animação dos dados

FLIGHT 3156

183.98 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 software2.00
Última ligação23/10/26-21:09:53
Sensor pressãoBosch BMP 581
Acelerómetro32G 3-axis
Giroscópio2000 dgps 3-axis

Flights from this altimeter

20 of 27

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 (417Hz)
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.
417 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 (44 samples / 109.42ms)
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.
Attitude filter 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
3156.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
899 KB
LOG
3156.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
101 KB
WX
3156_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 2026-10-23 14:00 local time at 31.9495, -108.5042.
1452 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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