By Topic

Interstellar Probe mission/system concept

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

3 Author(s)
Wallace, R.A. ; Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA ; Ayon, J.A. ; Sprague, G.A.

NASA's Interstellar Program was begun in the Spring of 1999 after a year of advanced mission and program planning activities, reported previously in a paper delivered at the 1999 IEEE Aerospace Conference. Summarized here is the progress towards defining the first mission in the Interstellar Program: Interstellar Probe (ISP). This mission will be the first to probe the interstellar medium with a complete set of scientific instruments designed for such exploration and is expected to be a precursor and a significant testbed for technologies being developed for eventual travel to the nearest star. Exploration of the interstellar medium is the objective of the Interstellar Probe mission. The interface between our solar system and galaxy defines the crossover into the interstellar medium and is the minimum target distance, thought to be beyond 125 AU. A mission requirement, therefore, is to reach 200 AU in fifteen years or less with a scientifically capable payload package. Time and distance are key design requirements, and advanced propulsion technology is a key enabler of the Interstellar Probe mission. Another key mission goal is to launch in the 2010 time period; thereby setting associated advanced technology goals of readiness by about 2007. Solar sail propulsion has been baselined for the mission design concept. Key trades are sail technology development requirements as a function of trip time to 200 AU and the payload mass that can be delivered and operated at that distance. This paper provides strawman payload and measurement requirements, technology and mission trade information, and a baseline system design, including a configuration concept. Alternate technology options are described

Published in:

Aerospace Conference Proceedings, 2000 IEEE  (Volume:7 )

Date of Conference: