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Prędkość
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Przyspieszenie
Wybierz jednostkę przyspieszenia: m/s² lub G
Lot 642

Flight 642

Mercury V1 Rev 1 · firmware 1.3
Apogeum
71.03m
4.25 s after launch
Maks. wznoszenie
37.14m/s
peak ascent
Maks. podczas spalania
7.37G
during the burn
Lądowanie
5.28s
touchdown 0.26 m/s
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Podsumowanie lotu

The flight, moment by moment

Liftoff
0 s
Nachylenie rampy2.47°
Thrust calc pad tilt7.3°
Launch detected
0.754 s
Wysokość25.43 m
Prędkość36.64 m/s
Wypalenie (pierwszy)
1.37 s
Wysokość40.39 m
Prędkość15.150 m/s
Apogeum
4.25 s
Wysokość71.03 Metry
Maks. nachylenie do wypalenia16.68°
Možliwy wyrzut
4.933 s
i
This ejection time was detected by the website from the accelerometer data, because the firmware did not record one for this flight.
Wysokość-0.27 m
Prędkość-0.43 m/s
Lądowanie
5.28 s
Wysokość62.7 m
Maks. opadanie-6.51 m/s

Stabilność69.9%Umiarkowany

Nachylenie przy wypaleniu (20%)81.5
20% · Launch tilt 7.3°
Prędkość pochylania/odchylania (30%)82.7
25% · Coning 45.6/54.1°/s
Coning · boost (25%)77.3
25% · Spin 380.6°/s
Prostoliniowość ciągu (15%)45.2
30% · Thrust 88%

Rocket information

Calculated from the flight data alone
Boost acceleration11.1 m/s²
average over the burn · 1.1 g
Coast deceleration5.3 m/s²
average · gravity plus drag
Apogee lost to tilt0.57 m
flown vertical ≈ 71.6 m · from the thrust-calculated tilt
Chute opening peak10.2 G
largest deceleration after ejection
Bateria & temperatura 0% → 0% · Temperatura początek 15.43 → 15.61 °C · Start po włączeniu 11m 38s

About the stability score

Worked out from the flight log between liftoff and 80% of apogee. It is independent of the angle the altimeter was mounted at, so it measures the flight rather than the fitting.

Nachylenie przy wypaleniu (20%)20%How close to vertical it left the rod.
Prędkość pochylania/odchylania (30%)25%How much the nose swung off the rocket's own axis across the whole ascent.
Coning · boost (25%)25%The same swing during the burn, when it matters most.
Prostoliniowość ciągu (15%)30%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 figures beside the score are the raw measurements behind these four.

Wysokość
Apogeum71.03 Metry
Czas do apogeum4.25 s
Wysokość wypalenia40.39 m
Wys. maks. prędkości12.79 m
Wys. wyrzutu-0.27 m
Wys. lądowania62.7 m
Wysokość nagrywania105.04 m
Prędkość
Maks. wznoszenie37.14 m/s
Maks. opadanie-6.51 m/s
Przy wypaleniu15.150 m/s
Prędk. opadania-0.348 m/s
Prędk. wyrzutu-0.43 m/s
Prędk. lądowania-0.255 m/s
Przyspieszenie
Maks. podczas spalania7.37 G
Maks. wznoszenie7.37 G
Maks. opadanie10.2 G
Śr. wznoszenie0 G
Śr. spalanie1.83 G
Czasy
Wypalenie (pierwszy)1.37 s
Apogeum4.25 s
Možliwy wyrzut4.933 s
Lądowanie5.28 s
Wyjście #1 WŁ0 s
Wyjście #1 WYŁ0 s
Kąty
Nachylenie rampy2.47°
Thrust calc pad tilt7.3°
Maks. nachylenie do wypalenia16.68°
Przechylenie startowe-2.36°
Pochylenie startowe-0.65°
Maks. obrót (spal.)1308.01 dps
Śr. obrót (spal.)609.14 dps
Recovery
Single deploy
No dual deploy detected on this flight.
Ogólne
Data przesłania02-Nov at 18:08
Próbki danych1066
Całkowity czas nagrania33.400 s
Śr. próbki/s31.9
Liczba blokad1
Start po włączeniu11m 38s
Oś referencyjnaX
Bateria & temperatura
Bateria początek0%
Bateria koniec0%
Temperatura początek15.43°C
Temperatura koniec15.61°C
Temp. MT1 startowa0°C
Reguły wyjścia
Brak skonfigurowanych reguł
Notatki užytkownika
Brak notatek
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Film Youtube
Brak filmu
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Zdjęcia lotu 0
Brak zdjęć
Silniki lotu
1st stage · 4s delay
1×B4-4KlimaDetails
Burn time
1.2 s
Diameter
18.00 mm
Average thrust
4 N
Max thrust
8 N
Total weight
16.30 g
Propellant weight
5.40 g
Propellant type
composite
Impulse5Ns
Max thrust8N
Burn time1.2s
Impulse classB
1st stage thrustloading curve…
Motor data by ThrustCurve.org
Dodaj to urządzenie do swojego konta, aby edytować
Powiązana rakieta
Žadna rakieta nie jest powiązana z tym lotem
Flight mass
Liftoff mass65.5gestimated
Mass at burnout60.1gestimated
No mass is set for this flight, so Motor thrust (N) uses a mass estimated from the measured burn and the motors’ rated impulse. Set the rocket’s mass for the measured impulse and specific impulse.
Motor thrust (N) is on the chart, under Acceleration.
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
Quest
B4~2
143
96%
91.5%
AeroTech
D15T
135
95.1%
94.2%
Quest
B6W
131
96.6%
92.8%
AeroTech
J520W
110
94%
92%
Loki
I405
100
93.5%
92.3%
AeroTech
G54
96
90.8%
85.3%
AeroTech
I245G
92
91.7%
94.1%
Loki
I377CT
88
92.9%
89.5%
Loki
G94IB
85
91.6%
89.6%
Quest
A3
83
95.3%
91.6%

Linked flights

Connect flights that belong together: a second altimeter flown in the same rocket, or the same rocket flown again. Linked flights appear on each other’s pages.

No linked flights yet.

Miejsce startu, data i godzina

Kliknij na mapę, aby oznaczyć miejsce startu. Przełączaj między widokiem mapy i satelity.

Imagery © Esri, Maxar, Earthstar Geographics

Kliknij na mapę · Przeciągnij, aby dostosować

Canopy height from the Meta and WRI High Resolution Canopy Height Maps v2 (Meta and World Resources Institute, 2026; source imagery © 2016 Vantor), used under CC BY 4.0. Ground elevation built from Terrain Tiles (Mapzen and AWS Open Data), derived from 3DEP and GMTED courtesy of the U.S. Geological Survey, SRTM courtesy of NASA, and ETOPO1 courtesy of NOAA. Map and imagery credited on the view above.

No launch site has been set for this flight.

Animacja danych lotu

FLIGHT 642

71.03 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.
Mercury V1
Revision 1
Mercury V1
Ten lot został wykonany na Mercury V1.
The hardware
Wersja sprzętuRev 1
Wersja oprogramowania1.3
Ostatnio online02-Nov at 18:12
Czujnik ciśnieniaBosch BMP 390
Akcelerometr32G 3-axis
Gyroskop2000 dgps 3-axis
MagnetometrN/A

Settings, as they were for this flight

Ogólne ustawienia lotu
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.
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.
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 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).
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.
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.
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.
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.
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 (9 samples / 281.00ms)
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.
1.4G
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
Wyjście 1 aktywne
i
Disable or enable the output from being able to turn on or off.
WYŁĄCZONY
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.
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.
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.
50.00 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.
0.00 °
Kalibracja czujników
Przesunięcia kalibracji użyte w tym locie.
Gyroskop⚠ Gyroskop nie został skalibrowany
X0.000°
Y0.000°
Z0.000°
Akcelerometr⚠ Akcelerometr nie został skalibrowany
X0.000 mG
Y0.000 mG
Z0.000 mG
Ustawienia urządzenia
TAG urządzenia
i
A custom name or tag assigned to this device for easy identification.
Merc8853
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+

Files

Where the altimeter signs its log, the file carries that signature and a tick beside it. A tick means the data is unchanged since the device wrote it, which is what a record claim needs.
CSV
642.csv
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
88 KB
Adjusted CSV2904 recalculated in your browser
The log recomputed for your own sea-level pressure and temperature. Columns: time, altitude as recorded and adjusted, raw altitude as recorded and adjusted, pressure.

This file is built here from the signed log, so it carries no signature of its own. Anyone verifying a claim should be sent to the flight page and build their own from the original.

Lot
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