Facts and figures


Proba liftoff
 
Proba liftoff onboard PSLV
 
 
Mission 
Launch date22 October 2001
Launch siteSriharikota, India
LauncherAntrix/ISRO PSLV-C3
OrbitLEO Sun-synchronous
Orbital parameters681x561 km
Orbital plane inclination97.9 degrees
Orbital period96.97 minutes
Mission durationOne year (planned)
Number of instrumentsEight
Number of technological payloadsSix
Mission operations and ground stationESA/REDU dedicated 2.4 m dish, average of 4 contacts of 10 m/day, automated evening & weekend passes
 
 
 
Proba during vibration tests
 
Proba PFM during vibration tests
 
 
Spacecraft 
Spacecraft mass94 kg
Instrument mass25 kg
Technological payload mass30 kg
Shape60x60x80 cm box shaped aluminium honeycomb structure
 
 
Proba-1 platform features
 
  • Computing system (highest performance computing system yet flown on an ESA spacecraft)
    • ERC-32 (SPARC V7) processor, >80 krad, 10 MIPS, 2 MFLOPS
    • TCS 21 020 digital signal processor, >100 krad, 15 MIPS, 45 MFLOPS
    • 12 other processors in subsystems/payload
    • off-the-shelf operating system (Vx Works)
    • full automatic code generation of all attitude control and navigation software (~50 000 lines of code)
  • 3-axis stabilisation (Earth pointing or inertial) by four miniaturised reaction wheels
    • absolute pointing accuracy: 150 arcsec
    • relative pointing stability: 10 arcsec over 10 s
  • 2-headed star tracker providing arcsec level pointing knowledge
     
     
    Sriharikota, India 8 February 2002
       
    Sriharikota, India - CHRIS image - 8 February 2002
     
  • GPS sensor providing 20 m position and fly-by knowledge

  • Spacecraft agility (along- and across-track), enabling multiple payload imaging (typically 5) of the same target in the same pass
    • Slew rate: up to 1 deg/s
  • Autonomous navigation via GPS and orbit propagation (no propulsion)

  • GaAs solar cells on five structure faces
    • 120 W peak
    • 17 W in safe mode
  • 28 Vdc regulated power bus
     
     
    The Mauna Kea volcano, Hawaii 15 April 2002
       
    Mauna Kea volcano, Hawaii - CHRIS image - 15 April 2002
     
  • 9 Ah Li-Ion battery

  • Passive thermal-control system

  • 1 Mbit/s S-band downlink

  • 4 kbit/s uplink

  • 1.2 Gbit data storage
     
     
     
    Last update: 27 May 2009


    In depth

     •  Third Party Missions: Proba-1 (http://earth.esa.int/missions/thirdpartymission/proba.html)
     •  Observing the Earth (http://www.esa.int/esaEO/index.html)
     •  Space Engineering (http://www.esa.int/SPECIALS/Space_Engineering/index.html)

    Related links

     •  Indian Space Research Organisation (http://www.isro.org/)
     •  Polar Satellite Launch Vehicle (http://www.isro.org/pslv.htm)