New Horizons [NASA]
New Horizons is a mission designed to fly by Pluto and its moon Charon and transmit images and data back to Earth. It will then continue on into the Kuiper Belt where it will fly by a number of Kuiper Belt Objects and return further data. The primary objectives are to characterize the global geology and morphology of Pluto and Charon, map the surface composition of Pluto and Charon, and characterize the neutral atmosphere of Pluto and its escape rate. Other objectives include studying time variability of Pluto's surface and atmosphere, imaging and mapping areas of Pluto and Charon at high-resolution, characterizing Pluto's upper atmosphere, ionosphere, and energetic particle environment, search for an atmosphere around Charon, refine bulk parameters of Pluto and Charon, search for additional satellites and rings, and characterize one or more Kuiper Belt Objects.
New Horizons is planned for launch in January 2006 by an Atlas-5(551) launch vehicle with additional Star-48B kick stage and will proceed to a Jupiter gravity assist in March 2007. (There are backup launch opportunities in February 2006 and February 2007.) The flyby will come within about 43 (+-5) Jovian radii of Jupiter and will be the center of a 4 month intensive Jupiter system observation campaign. The flyby will put the spacecraft on a trajectory towards Pluto, about 2.5 degrees out of the plane of the solar systems. During cruise to Pluto New Horizons may be targeted to fly by a Centaur object (an escaped Kuiper Belt Body) if a suitable target can be identified. Flyby of Pluto is expected in the summer 2016. The encounter period begins 6 months prior to closest approach. Long range imaging will include 40 km mapping of Pluto and Charon 3.2 days out. This is half the rotation period of Pluto-Charon and will allow imaging of the side of both bodies which will be facing away from the spacecraft at closest approach. New Horizons will fly within 9600 km of Pluto at a relative velocity of 11 km/s at closest approach and will come as close as 27,000 km to Charon. During the flyby the instruments should be able to obtain images with resolution as high as 25 m/pixel, 4-color global dayside maps at 1.6 km resolution, hyper-spectral near infrared maps at 7 km/pixel globally and 0.6 km/pixel for selected areas, characterization of the atmosphere, and radio science results. After passing by Pluto, New Horizons will be headed out to the Kuiper Belt where multiple Kuiper Belt Objects on the order of 50-100 km in diameter are expected to be targeted for encounter and similar measurements to those made at Pluto. This phase of the mission will last from 5 to 10 years.
The spacecraft has the shape of a thick triangle with a cyclindrical radiothermal generator (RTG) protruding from one vertex in the plane of the triangle and a 2.5 m radio dish antenna affixed to one flat side. Communication will be via X-band at a rate of 768 bps from Pluto to a 70-m DSN dish. The RTG will provide 174 W at encounter in 2016. Hydrazine monopropellant is used for propulsion, a delta-V capability of 290 m/s will be available after launch. The spacecraft has both 3-axis stabilized and spin-stabilized modes. Star cameras are mounted on the side of the spacecraft for navigation.
The spacecraft will carry four scientific instrument suites:
The closest encounter with Pluto happens on 14 July 2015. On 4 July, communications with the probe was lost for one hour and 21 minutes. The spacecraft detected the problem, switched to its backup computer and went into safe mode. The back-up system reinitiated communication with NASA's Deep Space Network. The rsolution of the problem and the return to nominal science operations might take a few days.
In August 2015, the target for the extended mission was selected. New Horizon will fly-by trans-neptunian asteroid 2014 MU69 on 1 January 2019.
|Type / Application:||Pluto flyby|
|Contractors:||Johns Hopkins University Applied Physics Laboratory (APL)|
|Equipment:||LORRI, MVIC, LEISA, ALICE, SWAP, PEPSSI, REX|
|Configuration:||spin or 3-axis stabilized body, high gain antenna, RTG|
|Propulsion:||Star-48B kick motor (jetisonable)|
|Lifetime:||10 - 15 years (primary mission)|
|Mass:||478 kg (without kick motor),|
|New Horizons (New Frontiers 1)||2006-001A||19.01.2006||CC SLC-41||Atlas-5(551) [Star-48B]|