Strona główna
Urządzenie: 1000-3BF4-4AA0
Lot ID: 1359
Podsumowanie lotu
Wysokość
Apogeum
135.6 Metry
Czas do apogeum
5.55 seconds
Wysokość wypalenia
58.82 m
Wys. maks. prędkości
44.67 m
Wys. wyrzutu
0.15 m
Wys. lądowania
-2.32 m
Stabilność
Wskaźnik stabilności
57.4 / 100 (Umiarkowany)
Rozkład stabilności
Nachylenie przy wypaleniu (20%)0
Stałość nachylenia (15%)42.5
Prędkość pochylania/odchylania (30%)73.4
Tłumienie (20%)80.7
Prostoliniowość ciągu (15%)85.5
Prędkość
Maks. wznoszenie
48.41 m/s
Maks. opadanie
0 m/s
Przy wypaleniu
44.320 m/s
Prędk. lądowania
-5.243 m/s
Prędk. opadania
-5.076 m/s
Prędk. wyrzutu
5.32 m/s
Recovery
Single deploy (no dual deploy detected)
Przyspieszenie
Maks. wznoszenie
6.69 G
Maks. opadanie
20.95 G
Maks. podczas spalania
6.69 G
Śr. wznoszenie
0 G
Śr. spalanie
1.27 G
Czasy
Wypalenie (pierwszy)
1.66 seconds
Apogeum
5.55 seconds
Možliwy wyrzut
0 seconds
Lądowanie
32.72 seconds
Kąty
Nachylenie rampy
97.89°
Maks. nachylenie do wypalenia
119.41°
Przechylenie startowe
99.13°
Pochylenie startowe
-30.15°
Maks. obrót (spal.)
204.8 dps
Śr. obrót (spal.)
69.47 dps
Ogólne
Data przesłania
22/03/26-11:01:41
Próbki danych
4294
Całkowity czas nagrania
45.107 s
Śr. próbki/s
95.1
Liczba blokad
0
Wysokość nagrywania
m
Start po włączeniu
0s
Oś referencyjna
Bateria & temperatura
Bateria początek
96%
Bateria koniec
96%
Temperatura początek
16.45°C
Temperatura koniec
16.2°C
Animacja danych lotu
FLIGHT 1359
135.6 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
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Notatki užytkownika
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Zdjęcia lotu (0)
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Powiązana rakieta
Žadna rakieta nie jest powiązana z tym lotem
Informacje o urządzeniu
Nano V1
Ten lot został wykonany na Nano V1.
Wersja sprzętu
Rev 4
Wersja oprogramowania
1.50
Ostatnio online
22/03/26-11:01:41
Czujnik ciśnienia
Bosch BMP 581
Akcelerometr
32G 3-axis
Gyroskop
2000 dgps 3-axis
Silniki lotu
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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Miejsce startu, data i godzina
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Lat—
Lng—
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Porównanie lotów
Comparing against 11 other flights with the same motor configuration.
Highest apogee
The maximum altitude reached. Higher is better for altitude-focused flights.
135.6m|199.39 best7th
Best stability
Composite score from tilt, spin rate, and ascent efficiency. 100 is perfect.
57.4/100|82.5 best5th
Fastest velocity
Peak ascent velocity recorded during the flight.
48.41m/s|61.1 best4th
Best avg burn G
Average acceleration during motor burn, in G-force.
1.27G|3.56 best9th
Longest flight
Total recording duration from launch to landing detection.
45.1s|52.3 best3rd
Lowest spin
Average spin rate during burn. Lower means a straighter flight.
69.47dps|53.82 best4th
Coldest flight
Board temperature at launch. Cold conditions affect battery and sensors.
0.16C|0.16 best1st
Is it in a tree?
How close landing altitude was to 8m above launch. Closer to 8m = more likely stuck in a tree!
8m|8 best1st
Spalanie silnika
To jest wielkość wyjściowa akcelerometru od startu do wypalenia.
You can check this against your motors thrust data on thrustcurve.org.
Ogólne ustawienia lotu
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Przejdź na stronę Moje urządzenia i skonfiguruj ustawienia..
Ciśnienie prognozowane
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
Detekcja startu
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.
25 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 300 or 600 samples stable or it will record until it's 10000 sample 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: 300 samples stable
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.
Kalman 1 (less)
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.
Disabled
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.
WŁĄCZONY
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.
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
Kalibracja czujników
Przesunięcia kalibracji użyte w tym locie.
Gyroskop
X
0.082°
Y
1.044°
Z
0.057°
Akcelerometr
X
224.710 mG
Y
4.850 mG
Z
14.470 mG
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