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Vuelo 2694

Yellow Alpha flight 59

Nano V1 Rev 4 · firmware 1.53
Apogeo
87.33m
5.1 s after launch
Máx. ascenso
212m/s
peak ascent
Máx. durante combustión
20.59G
during the burn
Aterrizaje
45.19s
touchdown 1.66 m/s
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Resumen del vuelo

The flight, moment by moment

Liftoff
0 s
Inclinación rampa14.10°
Thrust calc pad tilt1.8°
Fin combustión (primero)
1.05 s
Altitud29.88 m
Velocidad29.130 m/s
Launch detected
1.055 s
Altitud30.04 m
Velocidad29.04 m/s
Posible eyección
4.322 s
Altitud86.51 m
Velocidad1.08 m/s
Apogeo
5.1 s
Altitud87.33 Metros
Incl. máx. hasta fin comb.20.57°
Aterrizaje
45.18 s
Altitud0.52 m
Máx. descenso-5.03 m/s

Estabilidad85.1%Excelente

Inclinación al apagado (20%)95.2
20% · Launch tilt 1.8°
Cabeceo/guiñada (30%)86.9
25% · Coning 38.7/49.8°/s
Coning · boost (25%)80.1
25% · Spin 143.7°/s
Rectitud de empuje (15%)81.2
30% · Thrust 96%

Rocket information

Calculated from the flight data alone
Boost acceleration27.7 m/s²
average over the burn · 2.8 g
Coast deceleration7.2 m/s²
average · gravity plus drag
Apogee lost to tilt0.04 m
flown vertical ≈ 87.3 m · from the thrust-calculated tilt
Chute opening peak6.94 G
largest deceleration after ejection
Average descent rate2.1 m/s
ejection to landing · 40.86 s
Batería & temperatura 99% → 96% · Temperatura inicio 35.56 → 36.83 °C · Lanzamiento tras encendido 5m 49s

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
Apogeo87.33 Metros
Tiempo al apogeo5.1 s
Altitud fin combustión29.88 m
Altitud vel. máx.17.25 m
Altitud eyección86.51 m
Altitud aterrizaje0.52 m
Altitud grabación-15.73 m
Velocidad
Máx. ascenso212 m/s
Máx. descenso-5.03 m/s
En fin combustión29.130 m/s
Vel. descenso-2.075 m/s
Vel. eyección1.08 m/s
Vel. aterrizaje-1.661 m/s
Aceleración
Máx. durante combustión20.59 G
Máx. ascenso34.48 G
Máx. descenso6.94 G
Prom. ascenso1.03 G
Prom. combustión4.15 G
Tiempos
Fin combustión (primero)1.05 s
Apogeo5.1 s
Posible eyección4.322 s
Aterrizaje45.18 s
Ángulos
Inclinación rampa14.10°
Thrust calc pad tilt1.8°
Incl. máx. hasta fin comb.20.57°
Alabeo al lanzamiento1.97°
Cabeceo al lanzamiento13.81°
Giro máx. (comb.)1745.63 dps
Giro prom. (comb.)155.6 dps
Recovery
Single deploy
No dual deploy detected on this flight.
General
Fecha subida03/08/26-01:26:57
Muestras de datos6157
Tiempo total grabación74.600 s
Prom. muestras/s82.5
Número de bloqueos0
Lanzamiento tras encendido5m 49s
Eje de referenciaX
Batería & temperatura
Batería inicio99%
Batería fin96%
Temperatura inicio35.56°C
Temperatura fin36.83°C
Notas del usuario

Shock cord pulled out of mount, so post-ejection data is for 'chute, nose cone, shock cord and altimeter only. Body fell undamaged and was also recovered.

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Vídeo Youtube
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Imágenes del vuelo 0
Sin imágenes
Motores del vuelo
1st stage · 4s delay
1×A3-4EstesDetails
Burn time
1.01 s
Diameter
13.00 mm
Average thrust
2.2 N
Max thrust
5.83 N
Total weight
8.50 g
Propellant weight
3.30 g
Propellant type
black powder
Impulse2.22Ns
Max thrust5.8N
Burn time1.01s
Impulse classA
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Cohete vinculado
Ningún cohete vinculado a este vuelo
Flight mass
Liftoff mass41.8gestimated
Mass at burnout38.5gestimated
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.

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.

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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 siteLat47.702340Lng-122.139859Ground level10.0 m · 33 ftFecha lanzamiento2026-07-27Hora lanzamiento—
Animación de datos

FLIGHT 2694

87.33 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
Revision 4
Nano V1
Este vuelo se realizó con un Nano V1.
The hardware
Versión hardwareRev 4
Versión software1.53
Última conexión03/08/26-01:26:57
Sensor presiónBosch BMP 581
Acelerómetro32G 3-axis
Giroscopio2000 dgps 3-axis

Flights from this altimeter

10 of 10

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 (200Hz)
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.
24000
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.
200 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
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.
1.5G
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°
Y0.000°
Z0.000°
Acelerómetro⚠ El acelerómetro no ha sido 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
2694.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
456 KB
WX
2694_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 2026-07-27 12:00 local time at 47.7023, -122.1399.
136 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.

Vuelo
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