TY - GEN
T1 - Interstellar probe
T2 - 2005 IEEE Aerospace Conference
AU - Zurbuchen, T. H.
AU - Prashant, P.
AU - Gallimore, A.
AU - Scheeres, D.
AU - Murphy, N.
AU - Zank, G.
AU - Malhotra, R.
AU - Funsten, H.
PY - 2005
Y1 - 2005
N2 - 1,2The purpose of Interstellar Probe (ISP) is to follow NASA's exploratory mission to cross the heliospheric boundary regions and, for the first time, enter our extra-solar galactic environment. Interstellar Probe has therefore captured the imagination of the science community and the public for several decades. In 1999, NASA commissioned a science and technology definition team to address the science and technology aspects of ISP. A number of scientific issues and technology aspects have changed. We now also have modern three-dimensional simulations of the heliospheric interface regions. In addition, nuclear power has become a feasible alternative for propulsion of Interstellar Probe. We discuss how nuclear propulsion might affect the instrumentation, mission requirements, and mission plan, as well as how it may enable new science objectives. We discuss the science, payload, ongoing trade studies, and development of this approach for the Interstellar Probe, relying on technology developed for the Jupiter Icy Moon Orbiter (JIMO).
AB - 1,2The purpose of Interstellar Probe (ISP) is to follow NASA's exploratory mission to cross the heliospheric boundary regions and, for the first time, enter our extra-solar galactic environment. Interstellar Probe has therefore captured the imagination of the science community and the public for several decades. In 1999, NASA commissioned a science and technology definition team to address the science and technology aspects of ISP. A number of scientific issues and technology aspects have changed. We now also have modern three-dimensional simulations of the heliospheric interface regions. In addition, nuclear power has become a feasible alternative for propulsion of Interstellar Probe. We discuss how nuclear propulsion might affect the instrumentation, mission requirements, and mission plan, as well as how it may enable new science objectives. We discuss the science, payload, ongoing trade studies, and development of this approach for the Interstellar Probe, relying on technology developed for the Jupiter Icy Moon Orbiter (JIMO).
UR - http://www.scopus.com/inward/record.url?scp=33751534544&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=33751534544&partnerID=8YFLogxK
U2 - 10.1109/AERO.2005.1559397
DO - 10.1109/AERO.2005.1559397
M3 - Conference contribution
AN - SCOPUS:33751534544
SN - 0780388704
SN - 9780780388703
T3 - IEEE Aerospace Conference Proceedings
BT - Proceedings - 2005 IEEE Aerospace Conference
Y2 - 5 March 2005 through 12 March 2005
ER -