Afstand
Kies de afstandseenheid: Meter(m), Voet(ft), Mijl(mi) of Kilometer(km)
Snelheid
Kies de snelheidseenheid: m/s, ft/s, mph of km/h
Versnelling
Kies de versnellingseenheid: m/s² of G
Vlucht 2618

Flight 2618

Mercury Plus Rev 0 · firmware 1.00
Apogeum
178.68m
6.65 s after launch
Max. stijging
70m/s
peak ascent
Max. tijdens verbranding
8.48G
during the burn
Landing
20.79s
touchdown 20.45 m/s
ZOOM TO
s
s
Toon gebeurtenissen
Temp. & druk aanpassen ?
Afbeelding
Zoom
Klik en sleep, of knijp op mobiel
Vlucht vergelijken ?
Vluchtsamenvatting

The flight, moment by moment

Liftoff
0 s
Helling lanceerplatform5.84°
Thrust calc pad tilt0°
Launch detected
0.884 s
Hoogte50.22 m
Snelheid51.07 m/s
Uitbranding (eerste)
1.97 s
Hoogte79.88 m
Snelheid95.890 m/s
Apogeum
6.64 s
Hoogte178.68 Meter
Max. helling tot uitbranding7.80°
Mogelijke uitwerping
8.967 s
Hoogte154.57 m
Snelheid-18.2302912 m/s
Landing
20.78 s
Hoogte1.52 m
Max. daling-26.47 m/s

Stabiliteit0.1%Slecht

Helling bij burnout (20%)0
20% · Launch tilt 0°
Stamp/gier snelheid (30%)0
25% · Coning 0/0°/s
Coning · boost (25%)0
25% · Spin 0°/s
Stuwkrachtrechtheid (15%)0
30% · Thrust 0%

Rocket information

Calculated from the flight data alone
Boost acceleration48.7 m/s²
average over the burn · 5.0 g
Coast deceleration20.5 m/s²
average · gravity plus drag
Ballistic coefficient51 kg/m²
fitted to the 4.67 s coast
Chute opening peak348.11 G
largest deceleration after ejection
Average descent rate12.95 m/s
ejection to landing · 11.81 s
Batterij & temperatuur 86% → 83% · Temperatuur start 34.41 → 34.7 °C · Lancering na inschakelen 21m 20s

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.

Helling bij burnout (20%)20%How close to vertical it left the rod.
Stamp/gier snelheid (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.
Stuwkrachtrechtheid (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.

Hoogte
Apogeum178.68 Meter
Tijd tot apogeum6.64 s
Hoogte uitbranding79.88 m
Hoogte max. snelheid30.66 m
Hoogte uitwerping154.57 m
Hoogte landing1.52 m
Opnamehoogte225.41 m
Snelheid
Max. stijging70 m/s
Max. daling-26.47 m/s
Bij uitbranding95.890 m/s
Snelheid daling-28.757 m/s
Snelheid uitwerping-18.2302912 m/s
Snelheid landing-20.446 m/s
Versnelling
Max. tijdens verbranding8.48 G
Max. stijging8.48 G
Max. daling348.11 G
Gem. stijging0.27 G
Gem. verbranding2.87 G
Tijden
Uitbranding (eerste)1.97 s
Apogeum6.64 s
Mogelijke uitwerping8.967 s
Landing20.78 s
Uitgang #1 AAN0 s
Uitgang #1 UIT0 s
Hoeken
Helling lanceerplatform5.84°
Thrust calc pad tilt0°
Max. helling tot uitbranding7.80°
Rol bij lancering-1.57°
Stamp bij lancering5.62°
Max. rotatie (verbr.)543.71 dps
Gem. rotatie (verbr.)179.97 dps
Recovery
Single deploy
No dual deploy detected on this flight.
Algemeen
Uploaddatum20-Jul at 01:19
Datapunten5503
Totale opnametijd39.700 s
Gem. monsters/s138.6
Aantal vergrendelingen1
Lancering na inschakelen21m 20s
Referentie-asX
Batterij & temperatuur
Batterij start86%
Batterij einde83%
Temperatuur start34.41°C
Temperatuur einde34.7°C
Temp. MT1 lancering0°C
Gebruikersnotities
Geen notities
Voeg dit apparaat toe aan uw account om te bewerken
Youtube-video
Geen video
Voeg dit apparaat toe aan uw account om te bewerken
Vluchtafbeeldingen 0
Geen afbeeldingen
Vluchtmotoren
1st stage · 7s delay
1×E20W-7AeroTechDetails
Burn time
1.6 s
Diameter
24.00 mm
Average thrust
21.8 N
Max thrust
34.9 N
Total weight
49.00 g
Propellant weight
16.20 g
Propellant type
White Lightning
Impulse35Ns
Max thrust34.9N
Burn time1.6s
Impulse classE
1st stage thrustloading curve…
Motor data by ThrustCurve.org
Voeg dit apparaat toe aan uw account om te bewerken
Gekoppelde raket
Geen raket gekoppeld aan deze vlucht
Flight mass
Liftoff mass504.9gestimated
Mass at burnout488.7gestimated
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.
Rule events
No output rules fired during this flight.
Motorkoppeling (BETA)
Nog in testmodus! We werken eraan om te bepalen welke motor is gebruikt.
Merk
Motor
Score
Vorm
Brand
Cesaroni
F51-BS
147
94.3%
97.7%
Cesaroni
H200-BS
147
95.4%
95.7%
AeroTech
I600R
147
94.3%
96.7%
Cesaroni
H255-BS
142
93.7%
97%
Loki
I426-LB
142
95.5%
97%
AeroTech
H219T
137
94.2%
98.3%
AeroTech
J825R
137
91.1%
97.4%
AeroTech
D24
136
94.5%
94.3%
AeroTech
E28T
136
92.6%
93.7%
Cesaroni
H233-RL
132
94.7%
95.3%

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.

Lanceerplaats, datum & tijd

Klik op de kaart om uw lanceerlocatie te markeren. Schakel tussen kaart- en satellietweergave.

Imagery © Esri, Maxar, Earthstar Geographics

Klik op de kaart · Sleep om aan te passen

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.

Site nameUnnamed siteLat43.143448Lng-83.796309Ground level218.6 m · 717 ftLanceerdatum2026-07-19Lanceertijd13:48
Vluchtdata-animatie

FLIGHT 2618

178.68 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.
Mercury Plus
Revision 0
Mercury Plus
Deze vlucht is gevlogen met een Mercury Plus.
The hardware
HardwareversieRev 0
Softwareversie1.00
Laatst online14-Oct at 18:12
DruksensorBosch BMP 390
Versnellingsmeter32G 3-axis
Gyroscoop2000 dgps 3-axis
MagnetometerN/A

Settings, as they were for this flight

Algemene vluchtinstellingen
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.
1018.6 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.
50 meters
Bemonsteringsfrequentie
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.
1:5 (hybrid, reduces after apogee)
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.
18000
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.
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.
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.
Kalman 2 (default)
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.
0.5 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.
INGESCHAKELD (5 samples / 37.00ms)
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.
DISABLED
Uitvoerinstellingen
Arm switch
i
When enabled, GP6 is a hardware arm switch — outputs and rules are held off until the switch is closed to ground.
DISABLED
Startup lockout
i
Outputs and rules are blocked for this many seconds after power-on while sensors settle. 0 = off.
None
Launch confirm delay
i
After launch is detected, outputs and rules won't fire until this many seconds have passed.
2 s
Altitude floor
i
Outputs and rules are blocked until the rocket is at least this height above the launch pad.
50 m
Custom dataset 1
i
User-defined expression evaluated per sample, available for charting.
—
Custom dataset 2
—
Sensorkalibratie
Kalibratie-offsets gebruikt voor deze vlucht.
Gyroscoop⚠ Gyroscoop is niet gekalibreerd
X0.000°
Y0.000°
Z0.000°
Versnellingsmeter⚠ Versnellingsmeter is niet gekalibreerd
X0.000 mG
Y0.000 mG
Z0.000 mG
Apparaatinstellingen
Apparaat-TAG
i
A custom name or tag assigned to this device for easy identification.
Merc9119
Taal
i
The language setting configured on the device.
🇬🇧 English
Afsluitmodus
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
LED-helderheid
i
The brightness level of the LED indicators on the Mercury. Lower values save battery.
20%
WiFi TX power
i
WiFi transmit power level. Higher gives better range but uses more battery.
2 dBm (low)
Slaapstand
i
Controls whether the device enters low-power sleep when idle.
Normal (sleep when idle)
Batterijmonitor
i
Monitors battery voltage during the flight.
DISABLED
Cloud group
i
The cloud group / category this flight is assigned to.
General use
GP6 / GP7 poorten
GP-poortbesturing was niet beschikbaar voor firmware 2.0
I2C PCA9685 Servoboard
GP-poortbesturing was niet beschikbaar voor firmware 2.0
Voorspelling en luchtremmen
Deze functie was niet beschikbaar voor versie 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
2618.csv
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
436 KB
WX
2618_weather.json.gz
The weather for 48 hours either side of the launch, within 15 km of the launch site: NOAA GFS every hour, at the surface and up to about 31 km, and the NOAA GEFS ensemble where this site holds it. JSON, gzip compressed. Weather data by Open-Meteo.com (CC BY 4.0) and NOAA. For 2026-07-19 13:48 local time at 43.1434, -83.7963.
212 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.

Vlucht
Reacties
Inloggen om te reageren.
Inloggen om te reageren.