SUBORBITAL DYNAMICS

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NEXT LAUNCH:

    MISSION LOG: 2023-2025

    LEO-1-9

    SUPERPRESSURE FLIGHTS

    LEO-1 11/2023 Kiruna, 2 hours test flight
    LEO-2 06/2024 Espoo, 4 hours test flight
    LEO-3 08/2024 Espoo, 14 hours long duration flight
    LEO-4 09/2024 Tampere, 60 hours long duration flight
    LEO-5 09/2024 Aura, 2 hours test flight
    LEO-6 09/2024 Aura, 7 hours long duration flight
    LEO-7 10/2024 Helsinki, 1 hour bursted flight
    LEO-8 11/2024 Tampere, 24 hours long duration flight
    LEO-9 05/2025 Tampere, 50 hours long duration flight

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    MISSION LOG: 2024-2025

    HIPP-31-33

    PRIMARY TARGET

    Testing & verifying FTU (Flight Termination Unit) systems:
    - Fully autonomous detaching
    - Full-duplex UHF comms    SECONDARY TARGET
    First considerations toward radiation tolerant stratospheric mission systems

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    MISSION LOG: 2023

    HIPP-26-30

    PRIMARY TARGET

    Testing & verifying LEO-class probe systems including:
    - Payload design
    - Power management with solar cells
    - Data logging & handling
    - Location determination through trilateration
    - Communications and telemetry through TTN
    - Alternative buoyancy mechanisms    SECONDARY TARGET
    Producing high-quality imagery through advanced optical instrumentation

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    Next Mission: 06-05-2023

    HIPP-26

    PRIMARY TARGET

    Testing flights for telemetry unit development

    PAYLOAD DESIGN

    TBD

    FORECAST

    Chance of favorable atmospheric conditions: 87%

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    MISSION LOG: 2021-2022

    HIPP-20-25

    PRIMARY TARGET

    Classified testing flights for telemetry unit development

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    MISSION LOG: 4-9-2021

    HIPP-19

    PRIMARY TARGET

    Testing of LEO-class transmitter over ThingsNetwork.
    Gain video of parachute deployment for development.
    Testing atmospheric freeze-drying of ham at the edge of space.

    PAYLOAD DESIGN

    Photonics Apparatus: Mobius MaxiFlight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-868S2R- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280Payload Recovery System: TRATR1Lift vehicle: Hwoyee 200g

    MISSION: PARTIAL SUCCESS

    Received continuous data stream from over 100 km away at Tallinn ground station. Video capture didn't succeed due to possible battery freezing. High-altitude cured ham was delicious.

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    MISSION LOG: 23-5-2021

    HIPP-18

    PRIMARY TARGET

    Receive first live photographs from the craft.
    Test Parachute Deployment System (PDS) further.

    PAYLOAD DESIGN

    Photonics Apparatus: Mobius MaxiFlight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-433s2- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280Payload Recovery System: TRATR1Lift vehicle: Hwoyee 200g

    MISSION: PARTIAL SUCCESS

    Received first ever live photograph from the vessel and verified parachute deployment at 5 km altitude. Delaying the deployment will reduce the distance of glide after burst.

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    MISSION LOG: 24-4-2021

    HIPP-17

    PRIMARY TARGET

    Undisclosed to the public.

    MISSION: SUCCESS

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    MISSION LOG: 2021-3-13

    HIGH-ALTITUDE PARTICLE PROBE: FLIGHT 16

    PRIMARY TARGET

    Test Parachute Deployment System & 360 Camera

    PAYLOAD DESIGN

    Photonics Apparatus: 360 SphereFlight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-433s2- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280- Parachute Deployment System (PDS)Payload Recovery System: TRATR1Lift vehicle: Hwoyee 200g

    MISSION: PARTIAL SUCCESS

    Telemetry was received after launch and photonics apparatus recorded flight until parachute deployment. However, deployment occurred in earlier stage than planned due to high angular momentum of the craft.

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    MISSION LOG: 2021-1-16

    HIGH-ALTITUDE PARTICLE PROBE: FLIGHT 15

    PRIMARY TARGET

    Test & verify equipment and telemetry-relay in near space weather conditions

    PAYLOAD DESIGN

    Photonics Apparatus: Mobius MaxiFlight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-433s2- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280Payload Recovery System: TRATR1Lift vehicle: Hwoyee 200g

    MISSION: PARTIAL SUCCESS

    Telemetry was received after launch, but during recovery mission signal was not re-established due to terrain obstructions. However, all flight data was logged and valid. Photonics apparatus had drop of voltage in battery cell due to low temperature in the capsule.

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    MISSION LOG: 2020-10-24

    HIGH-ALTITUDE PARTICLE PROBE: FLIGHT 14

    PRIMARY TARGET

    Test & verify equipment and telemetry-relay for upcoming ultra-high flight.

    PAYLOAD DESIGN

    Photonics Apparatus: Mobius MaxiFlight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-433s2- Cosmic Ray Detector: OV2640- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280Payload Recovery System: TRATR1Lift vehicle: Hwoyee 200g

    MISSION: SUCCESFUL

    Achieved continuous telemetry link with UHF LoRa modulation from launch to landing.

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    MISSION LOG: 2020-09-26

    HIGH-ALTITUDE PARTICLE PROBE: FLIGHT 13

    PRIMARY TARGET

    Test & verify equipment and telemetry-relay for upcoming ultra-high flight.

    PAYLOAD DESIGN

    Photonics Apparatus: Mobius MaxiFlight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-433s2- Cosmic Ray Detector: OV2640- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280Payload Recovery System: TRATR1Lift vehicle: Hwoyee 200g

    MISSION: SUCCESFUL

    Uninterrupted radio communication achieved and maintained during flight. LOS at 400 m above sea line. Tracking visualization done with Arcgis. Max distance to probe 88 km.

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    MISSION LOG: 2020-08-15

    HIGH-ALTITUDE PARTICLE PROBE: FLIGHT 12

    PRIMARY TARGET

    Test & verify equipment and telemetry-relay for upcoming ultra-high flight.

    PAYLOAD DESIGN

    Photonics Apparatus: Mobius MaxiCosmic Ray Detector: HIPP-CRD-808#16Flight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-433s2- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280Payload Recovery System: TRATR1Lift vehicle: Hwoyee 800g

    MISSION: SUCCESFUL

    Uninterrupted radio communication achieved and maintained during flight. LOS at 4000 m above sea level due to terrain obstruction. Maximum achieved height was 34 km. Continuous live flight path data was received and visualized with Arcgis.

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    MISSION LOG: 2020-05-30

    HIGH-ALTITUDE PARTICLE PROBE: FLIGHT 11

    PRIMARY TARGET

    Uninterruptible 2-way radio communication with the mission payload to the apex of flight trajectory at height of ~15 km.

    PAYLOAD DESIGN

    Photonics Apparatus: Mobius MaxiCosmic Ray Detector: HIPP-CRD-808#16Flight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-433s2- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280Payload Recovery System: TRATR1Lift vehicle: Hwoyee 200g

    MISSION: SUCCESFUL

    Telemetry downlink achieved and maintained. Flight time 78 minutes, distance from launch pad to landing site ~50 km. Burst altitude 13 922 m.

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    MISSION LOG: 2020-03-14

    HIGH-ALTITUDE PARTICLE PROBE: FLIGHT 10

    PRIMARY TARGET

    Testing data logger and LoRa-telemetry.

    PAYLOAD DESIGN

    Photonics Apparatus: Mobius MaxiFlight Computer core: ARM Cortex M0 with modules;- Comms: RFM96-433s2- Spatial Awareness Apparatus: XA1110- Barometric Sensoring: BME280Payload Recovery System: TRATR1Lift vehicle: Hwoyee 200g

    MISSION: SUCCESFUL

    Achieved telemetry feed from probe and got a decent video from photonics apparatus. Logger gathered altitude and temperature data for whole mission. Maximum altitude being a bit over 20 km.

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    MISSION LOG: 2019-11-16

    HIGH-ALTITUDE PARTICLE PROBE: FLIGHT 9

    PRIMARY TARGET

    Testing data logger in subzero weather conditions. Lift vehicle Hwoyee 800g.

    PAYLOAD DESIGN

    NONDICLOSED INFORMATION

    MISSION: SUCCESFUL

    Achieved telemetry feed from probe and got heap of video from photonics apparatus. Logger gathered altitude and temperature data during the whole flight. Max altitude 17 103 m.

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    MISSION LOG: 2016-2019

    HIPP-1-8

    PRIMARY TARGET

    Technology & conditions assessment flights for future missions comprising of:
    - Telemetry alternatives eg. from 3G to Iridium
    - Flight computer selection with COTS focus
    - Battery chemistry studies
    - Lift vehicle & payload mods
    - Flight path predicting
    - Varied payload recovery methods
    - Observation of near space environment effects on flight components

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