Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions
Joint Authors
Song, Young-Joo
Jin, Ho
Garick-Bethell, Ian
Source
Mathematical Problems in Engineering
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-16, 16 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-04-16
Country of Publication
Egypt
No. of Pages
16
Main Subjects
Abstract EN
As a part of early system design activities, trajectory characteristics for a lunar CubeSat impactor mission as a function of its release conditions are analyzed.
The goal of this mission is to take measurements of surface magnetic fields to study lunar magnetic anomalies.
To deploy the CubeSat impactor, a mother-ship is assumed to have a circular polar orbit with inclination of 90 degrees at a 100 km altitude at the Moon.
Both the in- and out-of-plane direction deploy angles as well as delta-V magnitudes are considered for the CubeSat release conditions.
All necessary parameters required at the early design phase are analyzed, including CubeSat flight time to reach the lunar surface, impact velocity, cross ranges distance, and associated impact angles, which are all directly affected by the CubeSat release conditions.
Also, relative motions between these two satellites are analyzed for communication and navigation purposes.
Although the current analysis is only focused on a lunar impactor mission, the methods described in this work can easily be modified and applied to any future planetary impactor missions with CubeSat-based payloads.
American Psychological Association (APA)
Song, Young-Joo& Jin, Ho& Garick-Bethell, Ian. 2015. Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions. Mathematical Problems in Engineering،Vol. 2015, no. 2015, pp.1-16.
https://search.emarefa.net/detail/BIM-1074452
Modern Language Association (MLA)
Song, Young-Joo…[et al.]. Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions. Mathematical Problems in Engineering No. 2015 (2015), pp.1-16.
https://search.emarefa.net/detail/BIM-1074452
American Medical Association (AMA)
Song, Young-Joo& Jin, Ho& Garick-Bethell, Ian. Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions. Mathematical Problems in Engineering. 2015. Vol. 2015, no. 2015, pp.1-16.
https://search.emarefa.net/detail/BIM-1074452
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1074452