Changes between Version 36 and Version 37 of TBR/UserApp/Space/Proba_2


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Timestamp:
Oct 31, 2018, 5:15:39 PM (12 months ago)
Author:
lukamag
Comment:

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  • TBR/UserApp/Space/Proba_2

    v36 v37  
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    18 {| border="1"
    19 |+ '''PROBA-2 Mission Parameters'''
     18'''PROBA-2 Mission Parameters'''
    2019|-
    21 |Sponsor:
    22 |ESA
    23 |-
    24 |Expected Life:
    25 |2 years
    26 |-
    27 |Primary Applications:
    28 |Sun observations; technology demonstration
    29 |-
    30 |Primary SLR Applications:
    31 |Precision orbit determination
    32 |-
    33 |COSPAR ID:
    34 |0905902
    35 |-
    36 |SIC Code:
    37 |8005
    38 |-
    39 |NORAD SSC Code:
    40 |36037
    41 |-
    42 |Launch Date:
    43 |02-Nov-2009
    44 |-
    45 |NP Bin Size:
    46 |15 seconds
    47 |-
    48 |RRA Diameter:
    49 |16 cm
    50 |-
    51 |RRA Shape:
    52 |hemispherical
    53 |-
    54 |Reflectors:
    55 |7 corner cubes
    56 |-
    57 |Orbit:
    58 |Sun-synchronous dusk-dawn
    59 |-
    60 |Altitude (mean):
    61 |757 km
    62 |-
    63 |Inclination:
    64 |98.445 degrees
    65 |-
    66 |Eccentricity:
    67 |0.00116-0.0025
    68 |-
    69 |Weight:
    70 |130 kg
    71 |}
     20||= Sponsor: =||||= Expected Life: =||||= Primary Applications: =||||= Primary SLR Applications: =||||= COSPAR ID: =||||= SIC Code: =||
     21||ESA||||2 years||||Sun observations; technology demonstration||||Precision orbit determination||||0905902||||8005||
     22
     23     
     24
     25||=NORAD SSC Code:=||||=Launch Date:=||||=NP Bin Size:=||||=RRA Diameter:=||||=RRA Shape:=||||=Reflectors:=||
     26||36037||||02-Nov-2009||||15 seconds||||16 cm||||hemispherical||||7 corner cubes||
     27
     28 
     29||Orbit:||||Altitude (mean):||||Inclination:||||Eccentricity:||||Weight:||
     30||Sun-synchronous dusk-dawn||||757 km||||98.445 degrees||||0.00116-0.0025||||130 kg||
     31
    7232= PROBA 2 MISSION SUMMARY =
    7333
     
    664624The following table provides an overview of existing PROBA missions performed by ESA.
    665625
    666 {| border="1"
    667 |+ PROBA Missions overview
    668 !  !! Proba II !! Proba V
    669 |-
    670 ! Launch
    671 | 11/2009 || Planned in 2012
    672 |-
    673 ! Mass
    674 |130 Kg
    675 |160 Kg
    676 |-
    677 !Size
    678 |600 x 700 x 850 mm
    679 |800 x 800 x 1000 mm
    680 |-
    681 ! Orbit
    682 | Altitude between 700 km and 800 km, Sun-synchronous, Inclination 98.298 degrees
    683 | Sun-synchronised polar orbit, 820 km, with a 10:30 AM local time at the descending node
    684 |-
    685 !Launcher
    686 |Rockot
    687 |To be decided – designed to be compatible with Vega, Soyuz or Falcon 1E launchers.
    688 |-
    689 !Power consumption
    690 |53–86 Watts
    691 |131.2 Watts
    692 |-
    693 !RF
    694 |S-band, 64 kbit/s uplink; 1 Mbit/s downlink
    695 |S-band TxRx: 5W BPSK; X-band Tx: 6 W filtered OQPSK; MMU= 16 Gbit
    696 |-
    697 !Nominal Life
    698 |2 years
    699 |2.5 years
    700 |-
    701 !Ground Station
    702 |Redu (Belgium)
    703 |Satellite’s mission control centre in Redu, Belgium
    704 |-
    705 !Developed by
    706 |Consortium led by QinetiQ Space nv of Belgium
    707 |OIP Space Systems
    708 |}
     626PROBA Missions overview
     627|| ||||Launch||||Mass||||Size||||Orbit||||Launcher||||Power consumption||||RF||||Nominal Life||||Ground Station||||Developed by||
     628||Proba II||||11/2009||||130 Kg||||600 x 700 x 850 mm||||Altitude between 700 km and 800 km, Sun-synchronous, Inclination 98.298 degrees||||Rockot||||53–86 Watts||||S-band, 64 kbit/s uplink; 1 Mbit/s downlink||||2 years||||Redu (Belgium)||||Consortium led by QinetiQ Space nv of Belgium||
     629||Proba V ||||Planned in 2012||||160 Kg||||800 x 800 x 1000 mm||||Sun-synchronised polar orbit, 820 km, with a 10:30 AM local time at the descending node ||||To be decided – designed to be compatible with Vega, Soyuz or Falcon 1E launchers.||||131.2 Watts||||S-band TxRx: 5W BPSK; X-band Tx: 6 W filtered OQPSK; MMU= 16 Gbit||||2.5 years||||Satellite’s mission control centre in Redu, Belgium||||OIP Space Systems||
    709630= External links =
    710631