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Lot 1695

Mini Hustler flight 30

Nano V1 Rev 4 · firmware 1.51
Apogeum
124.01m
5.78 s after launch
Maks. wznoszenie
41.65m/s
peak ascent
Maks. podczas spalania
9.13G
during the burn
Lądowanie
30.7s
touchdown 5.07 m/s
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Podsumowanie lotu

The flight, moment by moment

Liftoff
0 s
Nachylenie rampy22.99°
Thrust calc pad tilt3.4°
Launch detected
1.353 s
Wysokość30.24 m
Prędkość33.69 m/s
Wypalenie (pierwszy)
2.25 s
Wysokość64.58 m
Prędkość37.240 m/s
Apogeum
5.78 s
Wysokość124.01 Metry
Maks. nachylenie do wypalenia34.88°
Možliwy wyrzut
6.429 s
i
This ejection time was detected by the website from the accelerometer data, because the firmware did not record one for this flight.
Wysokość121.04 m
Prędkość-7.22 m/s
Lądowanie
30.7 s
Wysokość-1.49 m
Maks. opadanie-14.7 m/s

Stabilność92.7%Doskonały

Nachylenie przy wypaleniu (20%)91.4
20% · Launch tilt 3.4°
Prędkość pochylania/odchylania (30%)95.5
25% · Coning 21.4/25.1°/s
Coning · boost (25%)94
25% · Spin 67.2°/s
Prostoliniowość ciągu (15%)90.2
30% · Thrust 98%

Rocket information

Calculated from the flight data alone
Boost acceleration16.6 m/s²
average over the burn · 1.7 g
Coast deceleration10.5 m/s²
average · gravity plus drag
Ballistic coefficient152 kg/m²
fitted to the 3.53 s coast
Apogee lost to tilt0.21 m
flown vertical ≈ 124.2 m · from the thrust-calculated tilt
Chute opening peak17.01 G
largest deceleration after ejection
Average descent rate5.04 m/s
ejection to landing · 24.27 s
Bateria & temperatura 92% → 91% · Temperatura początek 21.79 → 22.12 °C · Start po włączeniu 16m 46s

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
Apogeum124.01 Metry
Czas do apogeum5.78 s
Wysokość wypalenia64.58 m
Wys. maks. prędkości50.88 m
Wys. wyrzutu121.04 m
Wys. lądowania-1.49 m
Wysokość nagrywania-28.99 m
Prędkość
Maks. wznoszenie41.64 m/s
Maks. opadanie-14.7 m/s
Przy wypaleniu37.240 m/s
Prędk. opadania-4.926 m/s
Prędk. wyrzutu-7.22 m/s
Prędk. lądowania-5.069 m/s
Przyspieszenie
Maks. podczas spalania9.13 G
Maks. wznoszenie9.13 G
Maks. opadanie17.01 G
Śr. wznoszenie0.15 G
Śr. spalanie1.7 G
Czasy
Wypalenie (pierwszy)2.25 s
Apogeum5.78 s
Možliwy wyrzut6.429 s
Lądowanie30.7 s
Kąty
Nachylenie rampy22.99°
Thrust calc pad tilt3.4°
Maks. nachylenie do wypalenia34.88°
Przechylenie startowe13.10°
Pochylenie startowe18.97°
Maks. obrót (spal.)129.38 dps
Śr. obrót (spal.)74.23 dps
Recovery
Single deploy
No dual deploy detected on this flight.
Ogólne
Data przesłania07/06/26-20:33:04
Próbki danych3043
Całkowity czas nagrania39.234 s
Śr. próbki/s77.5
Liczba blokad0
Start po włączeniu16m 46s
Oś referencyjnaX
Bateria & temperatura
Bateria początek92%
Bateria koniec91%
Temperatura początek21.79°C
Temperatura koniec22.12°C
Notatki užytkownika
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Zdjęcia lotu 0
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Silniki lotu
1st stage · 5s delay
1×C6-5EstesDetails
Burn time
1.86 s
Diameter
18.00 mm
Average thrust
4.74 N
Max thrust
14.09 N
Total weight
24.10 g
Propellant weight
10.80 g
Propellant type
black powder
Impulse8.82Ns
Max thrust14N
Burn time1.86s
Impulse classC
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Flight mass
Liftoff mass137.8gestimated
Mass at burnout127gestimated
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.

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.

Site nameUnnamed siteLat47.705892Lng-122.139044Ground level10.0 m · 33 ftData startu2026-06-07Godzina startu12:15
Animacja danych lotu

FLIGHT 1695

124.01 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.
Nano V1
Revision 4
Nano V1
Ten lot został wykonany na Nano V1.
The hardware
Wersja sprzętuRev 4
Wersja oprogramowania1.51
Ostatnio online07/06/26-20:33:04
Czujnik ciśnieniaBosch BMP 581
Akcelerometr32G 3-axis
Gyroskop2000 dgps 3-axis

Flights from this altimeter

10 of 10

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.
1013.2 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.
30 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.
1:1:1 (100Hz)
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 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: 8s stable altitude
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.
TruePath
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.
Enabled (1/3 rate after apogee)
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 (31 samples / 330ms)
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.
1.5G
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⚠ Gyroskop nie został skalibrowany
X0.000°
Y0.000°
Z0.000°
Akcelerometr⚠ Akcelerometr nie został skalibrowany
X0.000 mG
Y0.000 mG
Z0.000 mG

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
1695.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
232 KB
WX
1695_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 2026-06-07 12:15 local time at 47.7059, -122.1390.
152 KB
Pobierz
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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