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Apparaat: 1000-3BF4-4B04
Vlucht ID: 1705Cosmic Cargo (2) flight 55
Toon gebeurtenissen
Downloaden
Temp. & druk aanpassen ?
Afbeelding
Datasets
Klik op de legenda om datasets te tonen of verbergen
Zoom
Klik en sleep, of knijp op mobiel
Vlucht vergelijken ?
Vluchtsamenvatting
Hoogte
Apogeum
138.38 Meter
Tijd tot apogeum
5.43 seconds
Hoogte uitbranding
31.05 m
Hoogte max. snelheid
35.47 m
Hoogte uitwerping
136.73 m
Hoogte landing
-0.76 m
Stabiliteit
Stabiliteitsscore
93.3 / 100 (Uitstekend)
Helling bij burnout (20%)93.5
Stamp/gier snelheid (30%)96.5
Coning · boost (25%)91.1
Stuwkrachtrechtheid (15%)92.2
Launch tilt 2.5° · Coning 18.7/31°/s · Spin 166.3°/s · Thrust 98.5%
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.
Helling bij burnout (20%) – how close to vertical it left the rod.
Stamp/gier snelheid (30%) and Coning · boost (25%) – how much the nose swung off the rocket's own axis. The main factor.
Stuwkrachtrechtheid (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.
Snelheid
Max. stijging
51.91 m/s
Max. daling
-17.13 m/s
Bij uitbranding
51.580 m/s
Snelheid landing
-9.252 m/s
Snelheid daling
-7.965 m/s
Snelheid uitwerping
4.16 m/s
Recovery
Single deploy (no dual deploy detected)
Versnelling
Max. stijging
14.45 G
Max. daling
25.98 G
Max. tijdens verbranding
11.18 G
Gem. stijging
0.66 G
Gem. verbranding
6.65 G
Tijden
Uitbranding (eerste)
0.81 seconds
Apogeum
5.43 seconds
Mogelijke uitwerping
5.006 seconds
i
This ejection time was detected by the website from the accelerometer data, because the firmware did not record one for this flight.
Landing
22.58 seconds
Hoeken
Helling lanceerplatform
15.46°
Thrust calc pad tilt
2.5°
Max. helling tot uitbranding
26.97°
Rol bij lancering
14.49°
Stamp bij lancering
0.81°
Max. rotatie (verbr.)
252.44 dps
Gem. rotatie (verbr.)
177.76 dps
Algemeen
Uploaddatum
09/06/26-00:04:19
Datapunten
2683
Totale opnametijd
32.519 s
Gem. monsters/s
82.5
Aantal vergrendelingen
0
Opnamehoogte
-10.68 m
Lancering na inschakelen
4m 2s
Referentie-as
X
Batterij & temperatuur
Batterij start
100%
Batterij einde
100%
Temperatuur start
29.04°C
Temperatuur einde
29.47°C
Vluchtdata-animatie
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
Opmerking: De vluchtanimatie vereist dat uw hoogtemeter in een vaste oriëntatie is gemonteerd. Kalibreer uw sensoren voor de beste resultaten.
Gebruikersnotities
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Vluchtafbeeldingen (0)
Geen afbeeldingen
Gekoppelde raket
Geen raket gekoppeld aan deze vlucht
Apparaatinformatie
Nano V1
Deze vlucht is gevlogen met een Nano V1.
Hardwareversie
Rev 4
Softwareversie
1.51
Laatst online
09/06/26-00:04:19
Druksensor
Bosch BMP 581
Versnellingsmeter
32G 3-axis
Gyroscoop
2000 dgps 3-axis
Vluchtmotoren
1st Stage
1x
Quest
B6W-4
Burn time
1.17 seconds
Diameter
18.00 mm
Average thrust
4.22 N
Max thrust
9.13 N
Impulse
4.87 Ns
Impulse class
B
Total weight
19.30 g
Propellant weight
2.80 g
Propellant type
White Lightning
Links
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Motorbrandduur
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).
Lanceerplaats, datum & tijd
Klik op de kaart om uw lanceerlocatie te markeren. Schakel tussen kaart- en satellietweergave.
No results found — try a different search.
Klik op de kaart · Sleep om aan te passen
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Vluchtvergelijking
Geen vluchten gevonden met dezelfde motorconfiguratie.
Algemene vluchtinstellingen
Dit is een momentopname van de instellingen die voor deze vlucht zijn gebruikt. Ga naar de
Ga naar de pagina Mijn apparaten en configureer de instellingen..
Voorspelde druk
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
Lanceerdetectie
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.
INGESCHAKELD (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.
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
Sensorkalibratie
Kalibratie-offsets gebruikt voor deze vlucht.
Gyroscoop
⚠ Gyroscoop is niet gekalibreerd
X
0.000°
Y
0.000°
Z
0.000°
Versnellingsmeter
⚠ Versnellingsmeter is niet gekalibreerd
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Reacties
Reacties
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