• → European Space Agency

      • Space for Europe
      • Space News
      • Space in Images
      • Space in Videos
    • About Us

      • Welcome to ESA
      • DG's News and Views
      • For Member State Delegations
      • Business with ESA
      • ESA Exhibitions
      • ESA Publications
      • Careers at ESA
    • Our Activities

      • Space News
      • Observing the Earth
      • Human Spaceflight
      • Launchers
      • Navigation
      • Space Science
      • Space Engineering
      • Operations
      • Technology
      • Telecommunications & Integrated Applications
    • For Public

    • For Media

    • For Educators

    • For Kids

    • ESA

    • YES2

    • Education

    • YES programme
    • The YES programme
    • About YES2
    • About YES2
    • Mission facts
    • Technical facts
    • Launch facts
    • Young engineers
    • Team overview
    • Meet the team
    • YES2 partners
    • YES2 partners
    • Centres of Expertise
    • YES2 deployment
    • Observe YES2
    • YES2 multimedia
    • Foton Mission Video-On-Demand
    • ESA Multimedia gallery
    • Image diary
    • Video clip
    • Press fact sheet
    • Presentation

    ESA > Education > Young Engineers Satellites

    Technical facts

    YES2

    YES2 has three components:

    • Fotino: a small 6 kg capsule which will return to Earth.

    • Mechanical data Acquisition Support System (MASS): an 8 kg carrier which holds Fotino in place with four straps. MASS will burn up in the atmosphere on re-entry.

    • Foton LOcated YES2 Deployer (FLOYD): a 22 kg carrier bolted onto Foton-M3, which will eject MASS and Fotino towards Earth. Inside FLOYD is a spool with 30 km of 0.5 mm thick Dyneema® tether which is connected to MASS.

    Dimensions 1020 x 410 x 475 (maximum envelope)
    Mass YES2 36 kg
    Mass Subsystem FLOYD 22 kg
    Mass Subsystem MASS 8 kg
    Mass Subsystem FOTINO 6 kg
    Operational duration 7 hours
    Ground Support • TsUP Russian Mission Control in Moscow (EMSR)
    • Payload Operation Centre in Kiruna (Sweden)
    Attitude Control required attitude allocated via Foton S/C (space craft)
    Telemetry • Telemetry system via Foton: unidirectional, data storage every 30s, max last 90min stored
    • Telemetry system via ESA Tele Support: bidirectional, 19200bps, storage every second
    Datalink MASS-FLOYD unidirectional UHF (ISM-band, 433 MHz), 9600 bps
    Power • 27V via Foton S/C, nominal operation 100Wh, peak 56W, average 24W during tether deployment
    • MASS/FLOYD autonomous
    Thermal Control passive thermal insulation, active control for OBC (on-board computer)
    Propulsion no propulsion system; required ∆v for re-entry via tether momentum transfer
    Tether Dyneema® 30000m x 0.5mm (polyethylene)

    Rate this

    Views

    Share

    • Currently 0 out of 5 Stars.
    • 1
    • 2
    • 3
    • 4
    • 5
    Rating: 0/5 (0 votes cast)

    Thank you for rating!

    You have already rated this page, you can only rate it once!

    Your rating has been changed, thanks for rating!

    17
    facebook
    twitter
    reddit
    google plus
    digg
    tumbler
    digg
    blogger
    myspace
    • More information
      • YES2 deployment in pictures
        • Week 3 in pictures - The launch!
          • Week 3 in pictures - The launch! part 2
            • Week 2 in pictures
              • Week 1 in pictures
              • Web diary
              • Sites
                Sites

    Connect with us

    • RSS
    • Youtube
    • Twitter
    • Flickr
    • Google Buzz
    • Subscribe
    • App Store
    • LATEST ARTICLES
    • · CryoSat hits land
    • · Ariane 5 completes seven launches …
    • · Measuring skull pressure without t…
    • · Malargüe station inauguration
    • · The solar wind is swirly
    • FAQ

    • Jobs at ESA

    • Site Map

    • Contacts

    • Terms and conditions