Title :
From the Sun to Pluto
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fDate :
31 Oct-7 Nov 1998
Abstract :
A core piece of technology which is common amongst three missions described is the avionics system being developed under NASA´s Advanced Deep Space Systems Development Program (ADSSDP). One of the first deliveries from ADSSDP is the X2000 avionics architecture which includes the main engineering computing system, the attitude control sensors, the power electronics and the core software used to operate the spacecraft in ground test and in flight. The avionics hardware technology utilizes integration of functions among a set of multichip modules with standard interfaces to achieve lower production costs, power and mass. Additionally, the packaging density improvements allow the reduction of the shielding mass required for the survival of the Europa Orbiter electronics within the intense Jupiter radiation belts
Keywords :
Jupiter; Pluto; aerospace computing; avionics; space vehicle electronics; system buses; Jupiter radiation belts; NASA; Pluto; Sun; X2000 avionics architecture; attitude control sensors; avionics hardware technology; multichip modules; packaging density; power electronics; shielding mass; standard interfaces; Aerospace electronics; Aerospace engineering; Computer architecture; Electronic equipment testing; Pluto; Power engineering and energy; Space missions; Space technology; Sun; Systems engineering and theory;
Conference_Titel :
Digital Avionics Systems Conference, 1998. Proceedings., 17th DASC. The AIAA/IEEE/SAE
Conference_Location :
Bellevue, WA
Print_ISBN :
0-7803-5086-3
DOI :
10.1109/DASC.1998.739854
