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Strona główna
Urządzenie: M-N79-915C
Lot ID: 324
Podsumowanie lotu
Wysokość
Apogeum
276.73 Metry
Czas do apogeum
7.49 seconds
Wysokość wypalenia
126.05 m
Wys. maks. prędkości
96.42 m
Wys. wyrzutu
275.81 m
Wys. lądowania
8.27 m
Stabilność
Wskaźnik stabilności
92.9 / 100 (Doskonały)
Rozkład stabilności
Nachylenie przy wypaleniu (20%)100
Stałość nachylenia (15%)92
Prędkość pochylania/odchylania (30%)81.6
Tłumienie (20%)100
Prostoliniowość ciągu (15%)98
Prędkość
Maks. wznoszenie
89.74 m/s
Maks. opadanie
-10.73 m/s
Przy wypaleniu
68.030 m/s
Prędk. lądowania
-6.550 m/s
Prędk. opadania
-6.882 m/s
Prędk. wyrzutu
4.52 m/s
Recovery
Single deploy (no dual deploy detected)
Przyspieszenie
Maks. wznoszenie
9.99 G
Maks. opadanie
6.59 G
Maks. podczas spalania
9.99 G
Śr. wznoszenie
0.03 G
Śr. spalanie
4.21 G
Czasy
Wypalenie (pierwszy)
1.93 seconds
Apogeum
7.49 seconds
Možliwy wyrzut
6.853 seconds
Lądowanie
46.46 seconds
Wyjście #1 WŁ
0 seconds
Wyjście #1 WYŁ
0 seconds
Kąty
Nachylenie rampy
5.54°
Maks. nachylenie do wypalenia
1.38°
Przechylenie startowe
1.27°
Pochylenie startowe
-5.37°
Maks. obrót (spal.)
144.75 dps
Śr. obrót (spal.)
100.35 dps
Ogólne
Data przesłania
10-Jul at 10:18
Próbki danych
1967
Całkowity czas nagrania
60.800 s
Śr. próbki/s
32.3
Liczba blokad
0
Wysokość nagrywania
-29.36 m
Start po włączeniu
0s
Oś referencyjna
Bateria & temperatura
Bateria początek
0%
Bateria koniec
0%
Temperatura początek
0°C
Temperatura koniec
0°C
Temp. MT1 startowa
0°C
Reguły wyjścia
Brak skonfigurowanych reguł
Animacja danych lotu
FLIGHT 324
276.73 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
Uwaga: Animacja lotu wymaga montażu wysokościomierza w stałej orientacji. Skalibruj czujniki dla najlepszych wyników.
Notatki užytkownika
Test rocket flight on a Klima D9 motor on a slightly modified Klima Pegasus rocket.
It did land in the tree just by the launch pad, so at least we know how high the tree is now!
It did land in the tree just by the launch pad, so at least we know how high the tree is now!
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Film Youtube
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Zdjęcia lotu (0)
Brak zdjęć
Powiązana rakieta
Žadna rakieta nie jest powiązana z tym lotem
Informacje o urządzeniu
Mercury V1
Ten lot został wykonany na Mercury V1.
Wersja sprzętu
Rev 1
Wersja oprogramowania
1.2B
Ostatnio online
30-Mar at 18:18
Akcelerometr
32G 3-axis
Gyroskop
2000 dgps 3-axis
Czujnik ciśnienia
Bosch BMP 390
Magnetometr
N/A
Silniki lotu
1st Stage
1x
Klima
D9-5
Burn time
2.10 seconds
Diameter
18.00 mm
Average thrust
9.00 N
Max thrust
25.00 N
Impulse
20.00 Ns
Impulse class
D
Total weight
27.10 g
Propellant weight
16.10 g
Propellant type
composite
Links
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Miejsce startu, data i godzina
Kliknij na mapę, aby oznaczyć miejsce startu. Przełączaj między widokiem mapy i satelity.
No results found — try a different search.
Kliknij na mapę · Przeciągnij, aby dostosować
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Reguły wyjścia
Reguły wyjścia were not available until firmware 2.0
Dopasowanie silnika (BETA)
Wciąż w trybie testowym! Pracujemy nad ustaleniem, jaki silnik był użyty.
Marka
Silnik
Wynik
Kształt
Spalanie
Contrail
G300
68
92.3%
79.6%
Estes
1/4A3T
12
-0.2%
44.2%
Estes
1/2A6
0
-24.4%
41.4%
Cesaroni
25-E75-VM-17A
0
58.3%
64.7%
Cesaroni
68-F240-VM-15A
0
50.1%
61.5%
AeroTech
H669N
0
79.4%
57.7%
Porównanie lotów
Comparing against 2 other flights with the same motor configuration.
Highest apogee
The maximum altitude reached. Higher is better for altitude-focused flights.
276.73m|276.73 best1st
Best stability
Composite score from tilt, spin rate, and ascent efficiency. 100 is perfect.
92.9/100|92.9 best1st
Fastest velocity
Peak ascent velocity recorded during the flight.
89.74m/s|89.74 best1st
Best avg burn G
Average acceleration during motor burn, in G-force.
4.21G|4.21 best1st
Longest flight
Total recording duration from launch to landing detection.
60.8s|74.4 best3rd
Lowest spin
Average spin rate during burn. Lower means a straighter flight.
100.35dps|91 best2nd
Coldest flight
Board temperature at launch. Cold conditions affect battery and sensors.
0C|0 best1st
Is it in a tree?
How close landing altitude was to 8m above launch. Closer to 8m = more likely stuck in a tree!
37.36m|37.36 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
To jest migawka ustawień użytych dla tego lotu. Przejdź na
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 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
Częstotliwość próbkowania
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:
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 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.
4x 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 3
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 2 (default)
Lockout time
i
The Lockout time is how long the altimeter should stop making decisions and taking actions if it detects unusual high speed altitude changes that are unexpected.
These false readings can be caused by ejection charges (if the altimeter is in the same compartment as the motor ejection gases) or even when you transition to Mach speeds and can give false readings of altitude changes.
When these events are detected the system enters Lockout for the specified time while it stabalises. This effects things like triggering the output, or calculating other data.
These false readings can be caused by ejection charges (if the altimeter is in the same compartment as the motor ejection gases) or even when you transition to Mach speeds and can give false readings of altitude changes.
When these events are detected the system enters Lockout for the specified time while it stabalises. This effects things like triggering the output, or calculating other data.
750ms
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.
1.5 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.
WŁĄCZONY (11 samples / 341.00ms)
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.
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.
Disabled
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.
Ustawienia wyjścia
To jest migawka ustawień użytych dla tego lotu.
Wyjście 1 aktywne
i
Disable or enable the output from being able to turn on or off.
WŁĄCZONY
Wyjście 1 wyzwalacz
i
After apogee (altitude)
This method triggers when the altitude drops below the set altitude after apogee is detected.After apogee (time)
This method triggers the defined seconds after apogee is detected.After launch (altitude)
This method is activated if/once the altimeter exceeds the set altitude after launch.After launch (time)
This option triggers the defined seconds after launch is detected.After burnout (time)
This method triggers the defined seconds after burnout is detected.
After apogee (altitude)
Wyjście 1 czas włączenia
i
This is how long the output should trigger ON state when the rules are met.
2000ms
Wyjście 1 wysokość
i
This is the altitude to trigger at if using a trigger method that works on altitude.
For example if you set this to 75m and After apogee (altitude) for the trigger then the output will turn on at 75m on descent above the launch altitude.
For example if you set this to 75m and After apogee (altitude) for the trigger then the output will turn on at 75m on descent above the launch altitude.
0 meters
Wyjście 1 czas
i
This is the time variable for output triggers that work on time.
For example if you set this to 3 seconds and After apogee (time) as the trigger then the output will turn on 3 seconds after apogee.
For example if you set this to 3 seconds and After apogee (time) as the trigger then the output will turn on 3 seconds after apogee.
0 seconds
Blokada wysokości
i
Altitude lock is a safety feature that prevents the output from triggering if the altitude is below this level when the rules are met.
0.00 m
Blokada kąta nachylenia
i
This is another safety feature. It can be used to disable the output if the rocket has gone too far from vertical.
For example if you set the tilt angle lock to 40 degrees then the output will not fire if the rocket is more than 40 degrees from vertical. To disable set this to 0.
For example if you set the tilt angle lock to 40 degrees then the output will not fire if the rocket is more than 40 degrees from vertical. To disable set this to 0.
0.00 °
Kalibracja czujników
Przesunięcia kalibracji użyte w tym locie.
Gyroskop
⚠ Gyroskop nie został skalibrowany
X
0.000°
Y
0.000°
Z
0.000°
Akcelerometr
⚠ Akcelerometr nie został skalibrowany
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Ustawienia urządzenia
To jest migawka ustawień użytych dla tego lotu.
To jest migawka ustawień użytych dla tego lotu.
TAG urządzenia
i
A custom name or tag assigned to this device for easy identification.
Merc2582
Język
i
The language setting configured on the device.
en
Tryb wyłączania
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
Jasność LED
i
The brightness level of the LED indicators on the Mercury. Lower values save battery.
WiFi TX power
i
WiFi transmit power level. Higher gives better range but uses more battery.
Tryb uśpienia
i
Controls whether the device enters low-power sleep when idle.
Stay awake
Monitor baterii
i
Monitors battery voltage during the flight.
ENABLED
Cloud group
i
The cloud group / category this flight is assigned to.
Porty GP6 / GP7
Sterowanie portami GP nie było dostępne przed firmware 2.0
Płytka servo I2C PCA9685
Sterowanie portami GP nie było dostępne przed firmware 2.0
Prognoza i hamulce powietrzne
Ta funkcja nie była dostępna przed wersją 2.10+
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