Distance
You can choose which units to use for distance from Meters(m), Feet(ft), Miles(mi) & Kilometers(km)
Velocity
You can pick which units to use for Velocity/speed such as Meters per second (m/s), Feet per second (ft/s), Miles per hour (mph) and Kilometers per hour (kph)
Acceleration
You can choose acceleration units to display from either Meters per second squared (m/s^2) or Gravity (G)
Flight 2618

Flight 2618

Mercury Plus Rev 0 · firmware 1.00
Apogee
178.68m
6.65 s after launch
Max ascent
70m/s
peak ascent
Max during burn
8.48G
during the burn
Landing
20.79s
touchdown 20.45 m/s
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Flight summary

The flight, moment by moment

Liftoff
0 s
Launch pad tilt5.84°
Thrust calc pad tilt0°
Launch detected
0.884 s
Altitude50.22 m
Velocity51.07 m/s
Burnout (first)
1.97 s
Altitude79.88 m
Velocity95.890 m/s
Apogee
6.64 s
Altitude178.68 Meters
Max tilt to burnout7.80°
Possible ejection
8.967 s
Altitude154.57 m
Velocity-18.2302912 m/s
Landing
20.78 s
Altitude1.52 m
Max descent-26.47 m/s

Stability0.1%Poor

Launch straightness (20%)0
20% · Launch tilt 0°
Coning · full (25%)0
25% · Coning 0/0°/s
Coning · boost (25%)0
25% · Spin 0°/s
Thrust straightness (30%)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
Battery & temperature 86% → 83% · Temperature start 34.41 → 34.7 °C · Launch after startup 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.

Launch straightness (20%)20%How close to vertical it left the rod.
Coning · full (25%)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.
Thrust straightness (30%)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.

Altitude
Apogee178.68 Meters
Time to apogee6.64 s
Burnout altitude79.88 m
Max velocity altitude30.66 m
Ejection altitude154.57 m
Landing altitude1.52 m
Recording altitude225.41 m
Velocity
Max ascent70 m/s
Max descent-26.47 m/s
At burnout95.890 m/s
Descent velocity-28.757 m/s
Ejection velocity-18.2302912 m/s
Landing velocity-20.446 m/s
Acceleration
Max during burn8.48 G
Max ascent8.48 G
Max descent348.11 G
Average ascent0.27 G
Average burn2.87 G
Times
Burnout (first)1.97 s
Apogee6.64 s
Possible ejection8.967 s
Landing20.78 s
Output #1 ON0 s
Output #1 OFF0 s
Angles
Launch pad tilt5.84°
Thrust calc pad tilt0°
Max tilt to burnout7.80°
Launch roll-1.57°
Launch pitch5.62°
Max spin (burn)543.71 dps
Avg spin (burn)179.97 dps
Recovery
Single deploy
No dual deploy detected on this flight.
General
Upload date20-Jul at 01:19
Data samples5503
Total recording time39.700 s
Average samples/s138.6
Number of lockouts1
Launch after startup21m 20s
Reference axisX
Battery & temperature
Battery start86%
Battery end83%
Temperature start34.41°C
Temperature end34.7°C
MT1 launch temp0°C
User notes
No notes added
Add this device to your account to edit
Youtube video
No video added
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Flight images 0
No images added
Flight motors
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
Add this device to your account to edit
Linked rocket
No rocket linked to this flight
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.
Motor match (BETA)
Very much in testing mode! We are working out how to guess which motor a flight flew on.
Brand
Motor
Score
Shape
Burn
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.

Launch site, date & time

Click anywhere on the map to mark your launch site. Switch between map and satellite view using the buttons below.

Imagery © Esri, Maxar, Earthstar Geographics

Click the map to place a marker · Drag to adjust

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 ftLaunch date2026-07-19Launch time13:48
Flight data animation

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

Note: Flight profile animation requires your altimeter to be mounted in a fixed orientation that you choose in your settings. For best results please calibrate your sensors as well.
Mercury Plus
Revision 0
Mercury Plus
This flight was flown on a Mercury Plus.
The hardware
Hardware versionRev 0
Software version1.00
Last online14-Oct at 18:12
Pressure sensorBosch BMP 390
Accelerometer32G 3-axis
Gyroscope2000 dgps 3-axis
MagnetometerN/A

Settings, as they were for this flight

General flight settings
Forecast pressure
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
Launch detect
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
Sample rate
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.
ENABLED (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
Output settings
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
—
Sensor calibration
Calibration offsets used during this flight.
Gyroscope⚠ Gyroscope has not been calibrated
X0.000°
Y0.000°
Z0.000°
Accelerometer⚠ Accelerometer has not been calibrated
X0.000 mG
Y0.000 mG
Z0.000 mG
Device settings
Device TAG
i
A custom name or tag assigned to this device for easy identification.
Merc9119
Language
i
The language setting configured on the device.
🇬🇧 English
Shutdown mode
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 brightness
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)
Sleep mode
i
Controls whether the device enters low-power sleep when idle.
Normal (sleep when idle)
Battery monitor
i
Monitors battery voltage during the flight.
DISABLED
Cloud group
i
The cloud group / category this flight is assigned to.
General use
GP6 / GP7 ports
GP port control was not available until firmware 2.0
I2C PCA9685 Servo Board
GP port control was not available until firmware 2.0
Prediction and air brakes
This feature was not available until version 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.

Flight
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