Distância
Escolha a unidade de distância: Metros(m), Pés(ft), Milhas(mi) ou Quilômetros(km)
Velocidade
Escolha a unidade de velocidade: m/s, ft/s, mph ou km/h
Aceleração
Escolha a unidade de aceleração: m/s² ou G
Voo 2782

Flight 2782

Mercury Plus Rev 0 · firmware 1.00
Apogeu
120.5m
6.08 s after launch
Máx. subida
44.69m/s
peak ascent
Máx. durante combustão
3.41G
during the burn
Aterragem
29.62s
touchdown 5.18 m/s
ZOOM TO
s
s
Mostrar eventos
Ajustar temp. & pressão ?
Imagem
Zoom
Clique e arraste, ou belisque no telemóvel
Comparar voo ?
Resumo do voo

The flight, moment by moment

Liftoff
0 s
Inclinação rampa2.27°
Thrust calc pad tilt0.9°
Launch detected
1.247 s
Altitude35.11 m
Velocidade39.11 m/s
Fim combustão (primeiro)
2.33 s
Altitude74.76 m
Velocidade29.770 m/s
Possível ejeção
5.442 s
Altitude120.31 m
Velocidade0.29 m/s
Apogeu
6.08 s
Altitude120.5 Metros
Incl. máx. até fim comb.11.29°
Aterragem
29.62 s
Altitude0.52 m
Máx. descida-8.11 m/s

Estabilidade94%Excelente

Inclinação no fim da queima (20%)97.6
20% · Launch tilt 0.9°
Taxa arfagem/guinada (30%)97
25% · Coning 17.3/15.2°/s
Coning · boost (25%)97.7
25% · Spin 71.6°/s
Retidão de empuxo (15%)86.1
30% · Thrust 97.1%

Rocket information

Calculated from the flight data alone
Boost acceleration12.8 m/s²
average over the burn · 1.3 g
Coast deceleration7.9 m/s²
average · gravity plus drag
Apogee lost to tilt0.01 m
flown vertical ≈ 120.5 m · from the thrust-calculated tilt
Chute opening peak208.63 G
largest deceleration after ejection
Average descent rate4.95 m/s
ejection to landing · 24.18 s
Bateria & temperatura 84% → 83% · Temperatura início 33.45 → 33.69 °C · Lançamento após arranque 9m 24s

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
Apogeu120.5 Metros
Tempo até apogeu6.08 s
Altitude fim combustão74.76 m
Altitude vel. máx.46.61 m
Altitude ejeção120.31 m
Altitude aterragem0.52 m
Altitude gravação200.41 m
Velocidade
Máx. subida44.69 m/s
Máx. descida-8.11 m/s
No fim combustão29.770 m/s
Vel. descida-4.870 m/s
Vel. ejeção0.29 m/s
Vel. aterragem-5.181 m/s
Aceleração
Máx. durante combustão3.41 G
Máx. subida3.41 G
Máx. descida208.63 G
Média subida0.24 G
Média combustão1.42 G
Tempos
Fim combustão (primeiro)2.33 s
Apogeu6.08 s
Possível ejeção5.442 s
Aterragem29.62 s
Saída #1 ON0 s
Saída #1 OFF0 s
Ângulos
Inclinação rampa2.27°
Thrust calc pad tilt0.9°
Incl. máx. até fim comb.11.29°
Rolagem no lançamento-2.12°
Arfagem no lançamento0.81°
Rotação máx. (comb.)146.9 dps
Rotação média (comb.)72.51 dps
Recovery
Single deploy
No dual deploy detected on this flight.
Geral
Data envio11-Aug at 19:13
Amostras de dados6290
Tempo total gravação44.200 s
Média amostras/s142.3
Número de bloqueios1
Lançamento após arranque9m 24s
Eixo de referênciaX
Bateria & temperatura
Bateria início84%
Bateria fim83%
Temperatura início33.45°C
Temperatura fim33.69°C
Temp. MT1 lançamento0°C
Notas do utilizador
Sem notas
Adicione este dispositivo à sua conta para editar
Vídeo Youtube
Sem vídeo
Adicione este dispositivo à sua conta para editar
Imagens do voo 1
Motores do voo
1st stage · 5s delay
1×C6-5EstesDetails
Burn time
1.86 s
Diameter
18.00 mm
Average thrust
4.74 N
Max thrust
14.09 N
Total weight
24.10 g
Propellant weight
10.80 g
Propellant type
black powder
Impulse8.82Ns
Max thrust14N
Burn time1.86s
Impulse classC
1st stage thrustloading curve…
Motor data by ThrustCurve.org
Adicione este dispositivo à sua conta para editar
Foguete associado
🚀
Active
Sizzler BT-60 Payloader for 18mm motors
1 flight linked
Type
Scratch built
Diameter
41.64mm
Dry weight
99.2g
Loaded wt.
140.2g
Mod
Modified
Stages
1
Fins
4
Recovery
Parachute
Chute
304cm
Body
Kraft paper
💬 No comments yet
Flight mass
Liftoff mass132.1gestimated
Mass at burnout121.3gestimated
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.
Rule events
No output rules fired during this flight.
Correspondência motor (BETA)
Ainda em modo de teste! Estamos a descobrir qual motor foi usado no voo.
Marca
Motor
Pontuação
Forma
Comb.
Contrail
J555
97
81.3%
84.8%
Contrail
I333
92
80.2%
78.5%
AeroTech
G76G
77
72.5%
80.7%
Loki
J474
72
72.7%
78.3%
Cesaroni
108-G68-WH-13A
69
28.4%
71.2%
Cesaroni
1633-K940-WT-18A
69
24.7%
70.1%
Contrail
H121
67
75.9%
78.7%
Contrail
I221
67
76%
83.4%
Cesaroni
1266-J760-WT-19A
64
24.6%
70%
Cesaroni
F32-WH
64
18.2%
68.8%

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.

Site nameUnnamed siteLat41.771721Lng-82.981593Ground level174.0 m · 571 ftData lançamento2026-08-11Hora lançamento13:07
Animação dos dados

FLIGHT 2782

120.5 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.
Mercury Plus
Revision 0
Mercury Plus
Este voo foi realizado num Mercury Plus.
The hardware
Versão hardwareRev 0
Versão software1.00
Última ligação14-Oct at 18:12
Sensor pressãoBosch BMP 390
Acelerómetro32G 3-axis
Giroscópio2000 dgps 3-axis
MagnetómetroN/A

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.
35 meters
Taxa amostragem
i
The base sample rate of the altimeter's sensors in samples per second. This setting was deprecated in firmware 2.0+.
32 Hz
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.
1:5 (hybrid, reduces after apogee)
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.
18000
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: 450 samples stable (~9s)
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.
Kalman 2 (default)
Lockout change
i
This is how we detect a lockout. If the pressure changes by this much in a single sample downwards (pressure increase, lower altitude) then it's likely to be a false reading. Multiply the setting by 32 to get the speed in meters per second that it will trigger at.
0.5 meters
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
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.
Upwards (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.
1.4G
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
Temp sensor
i
If an external MT1 temperature sensor is connected, this controls whether it is used for logging only or also for altitude calculations.
DISABLED
Definições de saída
Arm switch
i
When enabled, GP6 is a hardware arm switch — outputs and rules are held off until the switch is closed to ground.
DISABLED
Startup lockout
i
Outputs and rules are blocked for this many seconds after power-on while sensors settle. 0 = off.
None
Launch confirm delay
i
After launch is detected, outputs and rules won't fire until this many seconds have passed.
2 s
Altitude floor
i
Outputs and rules are blocked until the rocket is at least this height above the launch pad.
50 m
Custom dataset 1
i
User-defined expression evaluated per sample, available for charting.
—
Custom dataset 2
—
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
Definições do dispositivo
TAG dispositivo
i
A custom name or tag assigned to this device for easy identification.
Merc6352
Idioma
i
The language setting configured on the device.
🇬🇧 English
Modo encerramento
i
Controls what happens after recording. Standard shuts down normally, Delayed keeps WiFi on for 30 seconds after landing, Stay on keeps the device powered on.
Delayed 30s
Brilho LED
i
The brightness level of the LED indicators on the Mercury. Lower values save battery.
20%
WiFi TX power
i
WiFi transmit power level. Higher gives better range but uses more battery.
2 dBm (low)
Modo suspensão
i
Controls whether the device enters low-power sleep when idle.
Normal (sleep when idle)
Monitor bateria
i
Monitors battery voltage during the flight.
DISABLED
Cloud group
i
The cloud group / category this flight is assigned to.
General use
Portas GP6 / GP7
O controlo de portas GP não estava disponível até o firmware 2.0
Placa servo I2C PCA9685
O controlo de portas GP não estava disponível até o firmware 2.0
Previsão e freios aéreos
Esta funcionalidade não estava disponível até à versão 2.10+

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
2782.csv
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
527 KB
WX
2782_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 2026-08-11 13:07 local time at 41.7717, -82.9816.
602 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
Comentários
Iniciar sessão para comentar.
Iniciar sessão para comentar.