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Voo 1705

Cosmic Cargo (2) flight 55

Nano V1 Rev 4 · firmware 1.51
Apogeu
138.38m
5.43 s after launch
Máx. subida
51.91m/s
peak ascent
Máx. durante combustão
11.18G
during the burn
Aterragem
22.58s
touchdown 9.25 m/s
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Resumo do voo

The flight, moment by moment

Liftoff
0 s
Inclinação rampa15.46°
Thrust calc pad tilt2.3°
Launch detected
0.798 s
Altitude30.37 m
Velocidade51.54 m/s
Fim combustão (primeiro)
0.81 s
Altitude31.05 m
Velocidade51.580 m/s
Possível ejeção
4.894 s
i
This ejection time was detected by the website from the accelerometer data, because the firmware did not record one for this flight.
Altitude136.26 m
Velocidade4.16 m/s
Apogeu
5.43 s
Altitude138.38 Metros
Incl. máx. até fim comb.26.97°
Aterragem
22.58 s
Altitude-0.76 m
Máx. descida-17.13 m/s

Estabilidade93.4%Excelente

Inclinação no fim da queima (20%)94.1
20% · Launch tilt 2.3°
Taxa arfagem/guinada (30%)96.5
25% · Coning 18.7/31°/s
Coning · boost (25%)91.1
25% · Spin 166.3°/s
Retidão de empuxo (15%)92.2
30% · Thrust 98.5%

Rocket information

Calculated from the flight data alone
Boost acceleration63.7 m/s²
average over the burn · 6.5 g
Coast deceleration11.2 m/s²
average · gravity plus drag
Ballistic coefficient210 kg/m²
fitted to the 4.62 s coast
Apogee lost to tilt0.11 m
flown vertical ≈ 138.4 m · from the thrust-calculated tilt
Chute opening peak25.98 G
largest deceleration after ejection
Average descent rate7.74 m/s
ejection to landing · 17.69 s
Bateria & temperatura 100% → 100% · Temperatura início 29.04 → 29.47 °C · Lançamento após arranque 4m 2s

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
Apogeu138.38 Metros
Tempo até apogeu5.43 s
Altitude fim combustão31.05 m
Altitude vel. máx.35.47 m
Altitude ejeção136.26 m
Altitude aterragem-0.76 m
Altitude gravação-10.68 m
Velocidade
Máx. subida51.91 m/s
Máx. descida-17.13 m/s
No fim combustão51.580 m/s
Vel. descida-7.965 m/s
Vel. ejeção4.16 m/s
Vel. aterragem-9.252 m/s
Aceleração
Máx. durante combustão11.18 G
Máx. subida14.45 G
Máx. descida25.98 G
Média subida0.65 G
Média combustão6.18 G
Tempos
Fim combustão (primeiro)0.81 s
Apogeu5.43 s
Possível ejeção4.894 s
Aterragem22.58 s
Ângulos
Inclinação rampa15.46°
Thrust calc pad tilt2.3°
Incl. máx. até fim comb.26.97°
Rolagem no lançamento14.49°
Arfagem no lançamento0.81°
Rotação máx. (comb.)252.44 dps
Rotação média (comb.)177.76 dps
Recovery
Single deploy
No dual deploy detected on this flight.
Geral
Data envio09/06/26-00:04:19
Amostras de dados2683
Tempo total gravação32.519 s
Média amostras/s82.5
Número de bloqueios0
Lançamento após arranque4m 2s
Eixo de referênciaX
Bateria & temperatura
Bateria início100%
Bateria fim100%
Temperatura início29.04°C
Temperatura fim29.47°C
Notas do utilizador
Sem notas
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Vídeo Youtube
Sem vídeo
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Imagens do voo 0
Sem imagens
Motores do voo
1st stage · 4s delay
1×B6W-4QuestDetails
Burn time
1.17 s
Diameter
18.00 mm
Average thrust
4.22 N
Max thrust
9.13 N
Total weight
19.30 g
Propellant weight
2.80 g
Propellant type
White Lightning
Impulse4.87Ns
Max thrust9.1N
Burn time1.17s
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 mass76.5gestimated
Mass at burnout73.7gestimated
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.

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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 nameUnnamed siteLat47.705776Lng-122.139301Ground level10.0 m · 33 ftData lançamento2026-06-07Hora lançamento17:25
Animação dos dados

FLIGHT 1705

138.38 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 software1.51
Última ligação09/06/26-00:04:19
Sensor pressãoBosch BMP 581
Acelerómetro32G 3-axis
Giroscópio2000 dgps 3-axis

Flights from this altimeter

20 of 25

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 (100Hz)
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.
100 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 (1/3 rate after apogee)
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 (21 samples / 233ms)
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
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
1705.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
204 KB
WX
1705_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 2026-06-07 17:25 local time at 47.7058, -122.1393.
153 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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