STORK

Launching in June 2021, STORK is the innovative shared platform with Earth-Observation capabilities. Aimed at in-orbit services, the mission currently has capacity for external payloads. We add value to your business case by providing real-life service scenarios.
ico-amicalsat-01

Up to 2U of Cubesat capacity available

ico-swiatowid-03

Optical payload with up 5m resolution

ico-amicalsat-02

Earth-Observation services in-orbit and on the ground

Mission details

Our mission creates value in:
  • Image processing
  • Value-added Earth-Observation services
  • Demonstration of Earth-Observation technologies in real-life scenarios
  • Provision of services and data
Other uses:
  • In-orbit demonstration, verification and testing
  • Obtaining flight heritage
  • 6x of 0,25U slots
  • 3x of 0,5U slots
  • 1U + 0,5U slots
  • Tuna-can external slot
 
Space-proven NanoBus structure:
  • CNC manufactured of Aluminium 6061, 5083, 6082 alloy
  • Hard anodized and oxidized
  • Up to 2 safety deployment switches and 1 RBF pin
  • Two separation springs
 Available interfaces:
  • I2C, SPI, UART, RS485, RS422, CAN, USB, Ethernet, DAC/ADC
  • Other interfaces are available on request
 

Power management system is based on complex of Energy Harvesting System; Battery Management System; Auxiliary Power System (payload power supply). 

  • Peak power 75 W
  • System redundancy, autonomous fault handling and recovery
  • Battery supervisory circuit
  • Hardware protection from excessive discharge
  • Hardware MPPT implementation
  • User programable up to 6 A maximum battery pack load current
  • Available power supply: 1.8 V, 3.3 V, 5 V, 12 V and unregulated battery voltage
  • Main processor: up to 216 MHz, 2 MB FLASH
  • Storage memory: from 1 GB up to 16 GB NAND FLASH
  • External program memory: up to 3 MB with hardware Forward Error Correction
  • Payload interfaces: I2C, SPI, UART, RS485, RS422, CAN, USB, Ethernet, DAC/ADC
  • Multiple temperature sensors
  • Power supply: independent DC/DC converter
  • Over-The-Air update capability
Redundant low frequency communication module
 
  • Two independent radio transceivers
  • Frequency range: 400-440 MHz (optionally 120-500 MHz)
  • Transmission data rate 9,6 kb/s
  • RF output power: 30 dBm (reconfiguration available on request)
  • External program memory: up to 1 MB with hardware Forward Error Correction
  • Radio Sensitivity: -120 dBm
  • Over-The-Air update capability
S-band communication module
 
  • S-band frequency range: 2200 – 2290 MHz or 2400-2450 MHz
  • RF output power: 30 dBm
  • S-band transmission rate: 3.5 – 10.5 Mb/s
  • External program memory: up to 1 MB with hardware Forward Error Correction
  • Over-The-Air update capability
  • Space-proven advance flight computer
  • 3x magnetorquers
  • 3x reaction wheels
  • 1x coarse sun-sensor
  • 1x fine sun-sensor
  • 1x magnetometer 3-axis
  • 1x gyroscope 3-axis
  • 1x GPS receiver
  • Guaranteed platform accuracy: <1 degree of positioning accuracy; <1 degree of pointing accuracy

Platform is carrying SatRevolution Vision 300 optical payload with additional processing capabilities.

  • Bands: 3 (R, G, B)
  • Ground Sample Distance (GSD): 5.8 m @500 km
  • Field of View (FoV): 14.2 x 11.8 km @500 km; angle of view (AoV): 1.62° x 1.35°
  • Maximum image area per orbit: 3800 km2
  • Daily coverage: 61400 km2
  • On-board memory: FRAM 64 GB
  • Single image resolution: 2456 x 2054 px
  • Focal length: 300 mm; aperture – f/5.6
  • 8, 10, 12-bit processing
  • July-August 2020 – external payload design and readiness review
  • September-October 2020 – external payload design finalization
  • November 2020 – provision of payload engineering models
  • December 2020 – provision of payload flight models
  • January 2021 – payload integration
  • February-March 2021 – satellite integration and testing campaign
  • April 2021 – delivery for launch
  • June 2021 – launch to Sun-Synchronous orbit @500+ km altitude
  • July 2021-June 2024 – in-orbit service provision
  • Payload design review
  • Platform provision
  • Assembly, integration and testing
  • Campaign management
  • Launch event
  • Platform and payload commissioning
  • Payload in-orbit operations and service provision
To find out more about services aboard STORK mission please contact us



STORK mission platform visualization



STORK mission 3D model

STORK Mission

Interested in our services?

UNITED KINGDOM OFFICE

R71 Rutherford Appleton Laboratory
Harwell Campus
Didcot OPX11 0QX,
Oxfordshire, UK 

POLAND OFFICE

Stabłowicka 147
54-066 Wrocław
Poland

U.S.A. OFFICE

388 Market Street (Suite 1300)
San Francisco, CA 94111
United States

 

+48 533 325 851
contact@satrevolution.com