Hostname: page-component-77c89778f8-m42fx Total loading time: 0 Render date: 2024-07-19T05:12:26.502Z Has data issue: false hasContentIssue false

A Clementine II Mission to the Asteroids

Published online by Cambridge University Press:  12 April 2016

A.S. Hope
Affiliation:
Naval Research Laboratory, Washington, D.C., USA
B. Kaufman
Affiliation:
Naval Research Laboratory, Washington, D.C., USA
R. Dasenbrock
Affiliation:
Naval Research Laboratory, Washington, D.C., USA
D. Bakeris
Affiliation:
AlliedSignal Technical Services, Greenbelt, Maryland, USA

Abstract

Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.

Clementine II is a Department of Defense (DoD) and industry interplanetary mission designed to flyby several asteroids and release science probes that will impact these asteroids. Candidate asteroids were identified and a nominal and backup mission was chosen from these candidates. The mission design is discussed and the baseline encounters are presented. A backup mission is briefly described. A mass breakdown for the baseline mission is provided as well as the proposed mission sensors. The final encounter approach B-Plane errors are determined and analyzed. A final summary of the Clementine II mission is presented.

Type
Solar System Dynamics
Copyright
Copyright © Kluwer 1997

References

Bakeris, D., Hope, A., and Kaufman, B.: 1996, “Clementine II preliminary mission trajectory design”, SecondIAA International Conference on Low-Cost Planetary Missions, IAA-L-0205.Google Scholar
Middour, J.W., Dasenbrock, R.R., Kaufman, B., Hope, A.S., and Soyka, M.T.: 1995, “Clementine trajectory analysis”, CNES Spaceflight Dynamics Conference, Toulouse, France, CNES MS95/038Google Scholar
Nozette, S.:1995, “The Clementine mission”, Acta Astronautica, Suppl., 3, 161169.Google Scholar
Regeon, P.A., Chapman, R.J., and Baugh, R.: 1995, “Clementine - the Deep Space Program Science Experiment (DSPSE)”, Acta Astronautica, Suppl., 3, 307321.Google Scholar
Soyka, M.T.: 1995, “Clementine: contingency options for the phasing loops used in the Lunar transfer”, AAS/AIAA Spaceflight Mechanics Meeting, AAS 95-126.Google Scholar