Launch window 5-25 April 2023Earth-Moon flyby August 2024Venus flyby August 2025Earth flyby September 2026Earth flyby January 2029Arrival at Jupiter July 2031Ganymede orbit insertion December 2034Mission end late 2035
It's been a long time since I paid attention to this mission, but why does it take 8 years to get to Jupiter? Why did they have to do so many flybys? Galileo did it in 6 years with a Venus and Earth flyby. Cassini-Huygens reached Saturn in 7 years with two Venus, one Earth-Moon, and one Jupiter flyby.
Flybys of Jupiter's Moons:2 of Europa12 of Ganymede21 of Calisto
Quote from: GWR64 on 08/22/2021 07:25 amESA JUICE software, (I think, bohemian villages for me )https://www.cosmos.esa.int/web/spice/spice-for-juiceQuote5.0 New Baseline trajectory, launch September 2022same link updated:Quote 5.0b23.1 New Baseline trajectory, launch April 2023https://spiftp.esac.esa.int/data/SPICE/JUICE/kernels/mk/juice_crema_5_0b23_1.tmQuote - Launch on April, 5th 2023
ESA JUICE software, (I think, bohemian villages for me )https://www.cosmos.esa.int/web/spice/spice-for-juiceQuote5.0 New Baseline trajectory, launch September 2022
5.0 New Baseline trajectory, launch September 2022
5.0b23.1 New Baseline trajectory, launch April 2023
- Launch on April, 5th 2023
Quote from: Blackstar on 03/17/2022 08:58 pmIt's been a long time since I paid attention to this mission, but why does it take 8 years to get to Jupiter? Why did they have to do so many flybys? Galileo did it in 6 years with a Venus and Earth flyby. Cassini-Huygens reached Saturn in 7 years with two Venus, one Earth-Moon, and one Jupiter flyby.Most interplanetary missions launched by Ariane 5 take an extra year, even if the launcher performance is sufficient. The reason is that Ariane does not have a restartable second stage, as restarts are not needed for GTO launches from their near-equatorial site. Most interplanetary launches require a very specific DLA (the latitude over Earth where the escape firing needs to be to hit the target). Because the Earth's axis is tilted, and the solar system is not flat, this typically falls anywhere from +- 30 degrees from the equator.For a rocket that can re-start, this is no big deal. You launch into a parking orbit, wait until it's at the right latitude, then fire to escape velocity. But if your second stage cannot re-start, then the orbits you can achieve are limited to those where the latitude is quite close to that of your launch site. So what Ariane does is fire into an Earth-return orbit (which is accessible) a year early, and then do an flyby at the right latitude. This flyby adds no energy, but can reach orbits that direct ascent cannot. This is why Ariane 5 interplanetary missions almost always start with an Earth flyby one year after launch, where most other launchers go straight to their first flyby planet.I *think* something similar, but less serious, happened on one of the Chinese Mars missions. The launcher could reach the latitude they needed, but was not qualified for the length of coast required. So they could not quite aim straight at Mars, and had to do an extra maneuver on the way to reach it.
Our Jupiter Icy Moons Explorer @ESA_JUICE has a new launch window!Liftoff on an @ariane5 from Europe's Spaceport in Kourou during a 5-25 April 2023 window, starting an 8-year interplanetary cruise to the Jupiter system.Explore #Juice's journey 👉
And JUICE? "We will use the last Ariane 5 before the handover to Ariane 6," says Pham. "It will be launched from Kourou on the fifth of April 2023."Shipment to the launch facility is expected during January 2023
ESA's Jupiter Icy Moons Explorer (JUICE) mission will arrive at the gas giant planet in 2031 and make flybys of its moons Europa, Callisto and Ganymede. See highlights of the flight in this animation. Credit: ESA
I wish it reached Jupiter sooner, but alas. Guess we'll have to wait patiently
Is this the first interplanetary mission to use a lunar gravity assist? I know the STEREO spacecraft used lunar flybys to get into their different solar orbits, but any others that used it as part of a trajectory for a planetary target?