** PRE-LAUNCH PLANNING TRAJECTORY **
LAUNCH : Aug 7-27 2011 (Horizons trajectory: Aug 18, 2011 16:11:23 CT)
ARRIVE JUPITER: Aug 3, 2016 (JOI into 78-day capture orbit)
END OF MISSION: Oct 16, 2016 (de-orbits on apojove 33, Jupiter impact on periapse 34)
The Juno spacecraft (New Frontiers mission-class) will investigate Jupiter's origins, interior structure, deep atmosphere and magnetosphere, from a highly elliptical polar orbit with a close perijove (PJ=1.06 Jupiter-radii, AJ= 39 Jupiter-radii), using a suite of seven science instruments.
Main events:
Launch Aug 7-27 2011 (Horizons trajectory): 2011-Aug-18 16:11:23 CT
Deep space maneuvers (DSMs) : 2011-Jul-08 18:00 CT (365 m/s)
2011-Jul-10 18:00 CT (414 m/s)
Solar conjunction near DSM : 2012-Aug-14 20:50 CT (2.3 AU)
Earth flyby : 2013-Oct-12 09:19:55 CT @ 800 km alt.
Additional solar conjunctions on interplanetary phase:
: 2014-Aug-10 (3.4 AU)
: 2015-Sep-09 (5.0 AU)
Jupiter orbit insertion (JOI) (near perijove 0, into 78-day capture orbit):
: 2016-Aug-03 00:30 CT (480 m/s)
Period reduction maneuver (PRM) (near perijove 1):
: 2016-Oct-19 18:00 CT (592 m/s)
(PRM reduces period to "11-days" (~10.9725 days))
De-orbit maneuver at apojove 33 : 2017-Oct-11 07:34:32 CT (75 m/s)
Atmospheric impact : 2017-Oct-16 18:40:16 CT
SPACECRAFT PHYSICAL CHARACTERISTICS:
Solar-powered, spin-stablized spacecraft
1 rpm in interplanetary cruise, 2 rpm in Jupiter orbit
Three 2x9 m solar panels equally spaced around hexagonal bus (20 m span)
High-gain antenna
PROPULSION:
Bipropellant engine: Leros 1B, thrust= 635 N, Isp= 316.2 s min.
RCS thrusters
Orbit trim maneuvers (OTMs) occur on each orbit at perijove +4 hrs,
beginning at PJ3 (total ~38 m/s). Target desired longitude at descending node after perijove.
Total delta-V budget: 2107 m/s (~1852 m/s on bi-prop; remainder on RCS)