Osiris-rex frozen orbit design and flight experience

Daniel R. Wibben; Andrew Levine; Samantha Rieger; James V. McAdams; Peter G. Antreasian; Jason M. Leonard; Michael C. Moreau; Dante S. Lauretta

Osiris-rex frozen orbit design and flight experience

Daniel R. Wibben, Andrew Levine, Samantha Rieger, James V. McAdams, Peter G. Antreasian, Jason M. Leonard, Michael C. Moreau, Dante S. Lauretta

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

1 Scopus citations

Abstract

The OSIRIS-REx mission successfully entered a closed orbit around target asteroid Bennu for the first time on December 31, 2018. Due to the extremely low gravity of the asteroid, a specific orbit design was necessary to balance the perturbations provided from solar radiation pressure in order to maintain spacecraft safety, meet mission requirements, and demonstrate orbit stability over a propagation period of several months. This paper describes the design for OSIRIS-REx’s record-setting orbit and the as-flown performance of the spacecraft while it remained in orbit for two months without need for orbit maintenance.

Original language	English (US)
Title of host publication	AAS/AIAA Astrodynamics Specialist Conference, 2019
Editors	Kenneth R. Horneman, Christopher Scott, Brian W. Hansen, Islam I. Hussein
Publisher	Univelt Inc.
Pages	2959-2971
Number of pages	13
ISBN (Print)	9780877036654
State	Published - 2020
Event	AAS/AIAA Astrodynamics Specialist Conference, 2019 - Portland, United States Duration: Aug 11 2019 → Aug 15 2019

Publication series

Name	Advances in the Astronautical Sciences
Volume	171
ISSN (Print)	0065-3438

Conference

Conference	AAS/AIAA Astrodynamics Specialist Conference, 2019
Country/Territory	United States
City	Portland
Period	8/11/19 → 8/15/19

ASJC Scopus subject areas

Aerospace Engineering
Space and Planetary Science

Cite this

Wibben, D. R., Levine, A., Rieger, S., McAdams, J. V., Antreasian, P. G., Leonard, J. M., Moreau, M. C., & Lauretta, D. S. (2020). Osiris-rex frozen orbit design and flight experience. In K. R. Horneman, C. Scott, B. W. Hansen, & I. I. Hussein (Eds.), AAS/AIAA Astrodynamics Specialist Conference, 2019 (pp. 2959-2971). (Advances in the Astronautical Sciences; Vol. 171). Univelt Inc..

Osiris-rex frozen orbit design and flight experience. / Wibben, Daniel R.; Levine, Andrew; Rieger, Samantha et al.
AAS/AIAA Astrodynamics Specialist Conference, 2019. ed. / Kenneth R. Horneman; Christopher Scott; Brian W. Hansen; Islam I. Hussein. Univelt Inc., 2020. p. 2959-2971 (Advances in the Astronautical Sciences; Vol. 171).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Wibben, DR, Levine, A, Rieger, S, McAdams, JV, Antreasian, PG, Leonard, JM, Moreau, MC & Lauretta, DS 2020, Osiris-rex frozen orbit design and flight experience. in KR Horneman, C Scott, BW Hansen & II Hussein (eds), AAS/AIAA Astrodynamics Specialist Conference, 2019. Advances in the Astronautical Sciences, vol. 171, Univelt Inc., pp. 2959-2971, AAS/AIAA Astrodynamics Specialist Conference, 2019, Portland, United States, 8/11/19.

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abstract = "The OSIRIS-REx mission successfully entered a closed orbit around target asteroid Bennu for the first time on December 31, 2018. Due to the extremely low gravity of the asteroid, a specific orbit design was necessary to balance the perturbations provided from solar radiation pressure in order to maintain spacecraft safety, meet mission requirements, and demonstrate orbit stability over a propagation period of several months. This paper describes the design for OSIRIS-REx{\textquoteright}s record-setting orbit and the as-flown performance of the spacecraft while it remained in orbit for two months without need for orbit maintenance.",

author = "Wibben, \{Daniel R.\} and Andrew Levine and Samantha Rieger and McAdams, \{James V.\} and Antreasian, \{Peter G.\} and Leonard, \{Jason M.\} and Moreau, \{Michael C.\} and Lauretta, \{Dante S.\}",

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AU - Antreasian, Peter G.

AU - Leonard, Jason M.

AU - Moreau, Michael C.

AU - Lauretta, Dante S.

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AB - The OSIRIS-REx mission successfully entered a closed orbit around target asteroid Bennu for the first time on December 31, 2018. Due to the extremely low gravity of the asteroid, a specific orbit design was necessary to balance the perturbations provided from solar radiation pressure in order to maintain spacecraft safety, meet mission requirements, and demonstrate orbit stability over a propagation period of several months. This paper describes the design for OSIRIS-REx’s record-setting orbit and the as-flown performance of the spacecraft while it remained in orbit for two months without need for orbit maintenance.

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BT - AAS/AIAA Astrodynamics Specialist Conference, 2019

A2 - Horneman, Kenneth R.

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ER -

Osiris-rex frozen orbit design and flight experience

Abstract

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ASJC Scopus subject areas

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