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Dispositivo: 1000-3BF4-4B04
Vuelo ID: 1679Mini Hustler flight 25
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Resumen del vuelo
Altitud
Apogeo
125.7 Metros
Tiempo al apogeo
6.18 seconds
Altitud fin combustión
60.81 m
Altitud vel. máx.
51.1 m
Altitud eyección
125.7 m
Altitud aterrizaje
-0.99 m
Estabilidad
Puntuación estabilidad
93.8 / 100 (Excelente)
Inclinación al apagado (20%)95.9
Cabeceo/guiñada (30%)97.2
Coning · boost (25%)96.3
Rectitud de empuje (15%)87.7
Launch tilt 1.6° · Coning 16.9/19.5°/s · Spin 95.4°/s · Thrust 97.4%
About this score
Worked out from the flight log between liftoff and 80% of apogee, independent of the angle the altimeter was mounted at in the airframe.
Inclinación al apagado (20%) – how close to vertical it left the rod.
Cabeceo/guiñada (30%) and Coning · boost (25%) – how much the nose swung off the rocket's own axis. The main factor.
Rectitud de empuje (15%) – 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 line under the bars shows the raw measurements.
Velocidad
Máx. ascenso
39.28 m/s
Máx. descenso
-10.87 m/s
En fin combustión
37.600 m/s
Vel. aterrizaje
-4.897 m/s
Vel. descenso
-4.934 m/s
Vel. eyección
2.12 m/s
Recovery
Single deploy (no dual deploy detected)
Aceleración
Máx. ascenso
24.61 G
Máx. descenso
25.16 G
Máx. durante combustión
9.57 G
Prom. ascenso
0.2 G
Prom. combustión
1.97 G
Tiempos
Fin combustión (primero)
2.19 seconds
Apogeo
6.18 seconds
Posible eyección
6.183 seconds
i
This ejection time was detected by the website from the accelerometer data, because the firmware did not record one for this flight.
Aterrizaje
31.51 seconds
Ángulos
Inclinación rampa
26.73°
Thrust calc pad tilt
1.6°
Incl. máx. hasta fin comb.
47.82°
Alabeo al lanzamiento
-5.60°
Cabeceo al lanzamiento
26.16°
Giro máx. (comb.)
328.73 dps
Giro prom. (comb.)
102.37 dps
General
Fecha subida
02/06/26-22:51:54
Muestras de datos
3104
Tiempo total grabación
40.154 s
Prom. muestras/s
77.3
Número de bloqueos
0
Altitud grabación
-11.42 m
Lanzamiento tras encendido
5m 37s
Eje de referencia
X
Batería & temperatura
Batería inicio
72%
Batería fin
70%
Temperatura inicio
34.22°C
Temperatura fin
34.88°C
Animación de datos
FLIGHT 1679
125.7 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.
Notas del usuario
Mini Hustler flight 25. Four other altimeters aboard. Nominal flight.
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Vídeo Youtube
Sin vídeo
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Imágenes del vuelo (0)
Sin imágenes
Cohete vinculado
Ningún cohete vinculado a este vuelo
Información del dispositivo
Nano V1
Este vuelo se realizó con un Nano V1.
Versión hardware
Rev 4
Versión software
1.51
Última conexión
02/06/26-22:51:54
Sensor presión
Bosch BMP 581
Acelerómetro
32G 3-axis
Giroscopio
2000 dgps 3-axis
Motores del vuelo
1st Stage
1x
Estes
C6-5
Burn time
1.86 seconds
Diameter
18.00 mm
Average thrust
4.74 N
Max thrust
14.09 N
Impulse
8.82 Ns
Impulse class
C
Total weight
24.10 g
Propellant weight
10.80 g
Propellant type
black powder
Links
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Combustión del motor
The dashed line is the combined thrust curve for your motors (data from thrustcurve.org), scaled so its peak matches the recorded acceleration maximum — the shape is meaningful, the absolute level is not (your rocket's weight is unknown).
Sitio de lanzamiento, fecha y hora
Haga clic en el mapa para marcar su sitio de lanzamiento. Cambie entre vista de mapa y satélite.
No results found — try a different search.
Clic en el mapa · Arrastre para ajustar
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Comparación de vuelo
Comparing against 3 other flights with the same motor configuration.
Highest apogee125.7 m 1st of 4
The maximum altitude reached above the launch point.
you
best
best 125.7 m · you
Best stability93.8 /100 2nd of 4
How straight it flew: launch, coning and thrust straightness combined. 100 is perfect.
you
best
best 94.9 /100 · Mini Hustler flight 24 (#1678)
Fastest velocity39.28 m/s 2nd of 4
Peak ascent velocity recorded during the flight.
you
best
best 41.64 m/s · Mini Hustler flight 30 (#1695)
Best avg burn G1.06 G 2nd of 4
Average acceleration during the motor burn, in G.
you
best
best 1.1 G · Mini Hustler flight 24 (#1678)
Longest flight40.15 s 1st of 4
Total recording time from launch to landing.
you
best
best 40.15 s · you
Lowest spin102.37 dps 3rd of 4
Average spin rate during the burn.
you
best
best 74.23 dps · Mini Hustler flight 30 (#1695)
Coldest flight0.34 C 4th of 4
Board temperature at launch.
you
best
best 0.21 C · Mini Hustler flight 30 (#1695)
🌲 Is it in a tree?-0.99 m 2nd of 4
Just for fun: whichever flight came down closest to 8 m above the launch point (roughly tree height) is the one most likely stuck up a tree.
8 m
you
best
closest to 8 m · Mini Hustler flight 24 (#1678) at -0.99 m
Ajustes generales del vuelo
Esta es una captura de los ajustes utilizados para este vuelo. Visite la
Visite la página Mis dispositivos y configure los ajustes..
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.
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.
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 (50Hz)
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).
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.
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.
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.
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 1.0
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.
ACTIVADO (21 samples / 213ms)
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.
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
⚠ El giroscopio no ha sido calibrado
X
0.000°
Y
0.000°
Z
0.000°
Acelerómetro
⚠ El acelerómetro no ha sido calibrado
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Comentarios
Comentarios
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