DocumentCode :
2567468
Title :
Spacecraft and mission design of the `Aeneas´ Mercury orbiter using methods of concurrent engineering
Author :
Joseph, Steffy Maria ; Flowers-Jacobs, N.E. ; Jackson, R.P. ; Scott, K.J.
Author_Institution :
1683 Broadway #402, Ann Arbor, MI, USA
Volume :
7
fYear :
2000
fDate :
2000
Firstpage :
341
Abstract :
Over the course of ten weeks, nine college students collaborated to design a mission to Mercury. The Aeneas Mercury Orbiter was designed using new methods of concurrent engineering with the help of NASA´s Jet Propulsion Laboratory. Aeneas will deliver a significant scientific payload, including visual cameras, an altimeter, laser and infrared spectrometers, and magnetometers, to a difficult target to return information about the little known planet Mercury. After a three-year trajectory including a Venus flyby, the spacecraft will reach Mercury and begin a 300 km circular polar orbit. Expected science return includes visual mapping of at least 95% of the surface, mapping of the Mercurian magnetic field, and partial determination of the planetary surface. The Aeneas Mercury Orbiter will enhance current knowledge of the solar system and its formation through the study of Mercury
Keywords :
Mercury (planet); concurrent engineering; design engineering; planetary magnetism; space communication links; space research; space vehicles; terrain mapping; Aeneas Mercury Orbiter; Mercurian magnetic field mapping; Venus flyby; altimeter; circular polar orbit; concurrent engineering; infrared spectrometer; laser spectrometer; magnetometers; mission design; planetary probe; planetary surface mapping; scientific payload; spacecraft design; visual cameras; visual mapping; Cameras; Collaboration; Concurrent engineering; Design methodology; Educational institutions; Infrared spectra; Laboratories; Payloads; Propulsion; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-5846-5
Type :
conf
DOI :
10.1109/AERO.2000.879301
Filename :
879301
Link To Document :
بازگشت