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Apparaat: 1000-3BF4-4BE
Vlucht ID: 1719200Hz Nano test (1)
Toon gebeurtenissen
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Temp. & druk aanpassen ?
Afbeelding
Datasets
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Vlucht vergelijken ?
Vluchtsamenvatting
Hoogte
Apogeum
148.13 Meter
Tijd tot apogeum
4.44 seconds
Hoogte uitbranding
53.97 m
Hoogte max. snelheid
50.18 m
Hoogte uitwerping
147.97 m
Hoogte landing
112.3 m
Stabiliteit
Stabiliteitsscore
20.2 / 100 (Slecht)
Helling bij burnout (20%)82.5
Stamp/gier snelheid (30%)11.2
Coning · boost (25%)3.8
Stuwkrachtrechtheid (15%)0
Launch tilt 6.9° · Coning 281.4/502.6°/s · Spin 204.5°/s · Thrust 77.8%
⚠ Low confidence — altimeter may have moved in flight
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
52.72 m/s
Max. daling
-21.55 m/s
Bij uitbranding
51.280 m/s
Snelheid landing
-6.063 m/s
Snelheid daling
-4.769 m/s
Snelheid uitwerping
-0.62 m/s
Recovery
Single deploy (no dual deploy detected)
Versnelling
Max. stijging
8.63 G
Max. daling
42.8 G
Max. tijdens verbranding
8.63 G
Gem. stijging
-0.5 G
Gem. verbranding
0.84 G
Tijden
Uitbranding (eerste)
0.49 seconds
Apogeum
4.44 seconds
Mogelijke uitwerping
4.717 seconds
Landing
11.94 seconds
Hoeken
Helling lanceerplatform
19.89°
Thrust calc pad tilt
6.9°
Max. helling tot uitbranding
48.59°
Rol bij lancering
-15.12°
Stamp bij lancering
-9.73°
Max. rotatie (verbr.)
1260.33 dps
Gem. rotatie (verbr.)
678.92 dps
Algemeen
Uploaddatum
08/06/26-21:20:10
Datapunten
5871
Totale opnametijd
42.228 s
Gem. monsters/s
139
Aantal vergrendelingen
0
Opnamehoogte
81.03 m
Lancering na inschakelen
1m 4s
Referentie-as
X
Batterij & temperatuur
Batterij start
99%
Batterij einde
96%
Temperatuur start
20.64°C
Temperatuur einde
15.14°C
Vluchtdata-animatie
FLIGHT 1719
148.13 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
First test of the Nano altimeter at 200Hz for the new firmware. A small bug on the launch point look back but otherwise has worked rather well. The pre buffer scaling hasn't taken effect so there wasn't enough to have an accurate launch point or lookback, resolved with time based prebuffer rather than fixed sample number.
This flight was flown in the main tube exposed the ejection charge and out in the open air on descent. The True path filter has done a great job at cleaning up the noise and ejection charge pressure spike it would have seen.
This flight was flown in the main tube exposed the ejection charge and out in the open air on descent. The True path filter has done a great job at cleaning up the noise and ejection charge pressure spike it would have seen.
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Vluchtafbeeldingen (0)
Geen afbeeldingen
Gekoppelde raket
✅ Active
1
Klima Pegasus - Test Beast
Klima — Pegasus RTF
✈️ 2 flights linked
Type
Kit build
Diameter
35mm
Length
495mm
Dry weight
80g
Stages
1
Recovery
Parachute
Apparaatinformatie
Nano V1
Deze vlucht is gevlogen met een Nano V1.
Hardwareversie
Rev 4
Softwareversie
1.52
Laatst online
08/06/26-21:20:10
Druksensor
Bosch BMP 581
Versnellingsmeter
32G 3-axis
Gyroscoop
2000 dgps 3-axis
Vluchtmotoren
1st Stage
1x
Klima
C6-5
Burn time
1.60 seconds
Diameter
18.00 mm
Average thrust
6.00 N
Max thrust
15.00 N
Impulse
10.00 Ns
Impulse class
C
Total weight
20.50 g
Propellant weight
9.60 g
Propellant type
composite
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
Comparing against 13 other flights with the same motor configuration.
Highest apogee148.13 m 6th of 11
The maximum altitude reached above the launch point.
you
best
best 199.39 m · Flight #1246
Best stability20.2 /100 11th of 11
How straight it flew: launch, coning and thrust straightness combined. 100 is perfect.
you
best
best 93.5 /100 · Flight #1360
Fastest velocity52.72 m/s 4th of 11
Peak ascent velocity recorded during the flight.
you
best
best 61.1 m/s · Flight #1146
Best avg burn G2.68 G 9th of 11
Average acceleration during the motor burn, in G.
you
best
best 3.56 G · Flight #1246
Longest flight42.22 s 4th of 11
Total recording time from launch to landing.
you
best
best 52.3 s · Flight #1333
Lowest spin678.92 dps 11th of 11
Average spin rate during the burn.
you
best
best 53.82 dps · Flight #1333
🌲 Is it in a tree?112.3 m 5th of 11
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 · 200Hz Nano test (2) (#1734) at 2.38 m
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.
0
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.
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.
INGESCHAKELD
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
X
2.000°
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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