Entry, Descent, and Landing System Design for the Mars Gravity Biosatellite

dc.contributor.author Korzun, Ashley M. en_US
dc.contributor.author Smith, Brandon P. en_US
dc.contributor.author Yu, Chi-Yau en_US
dc.contributor.author Hartzell, Christine M. en_US
dc.contributor.author Hott, Kyle B. en_US
dc.contributor.author Place, Laura A. en_US
dc.contributor.author Braun, Robert D. en_US
dc.contributor.author Martinelli, Scott K. en_US
dc.contributor.corporatename Georgia Institute of Technology. School of Aerospace Engineering en_US
dc.date.accessioned 2009-01-20T20:15:07Z
dc.date.available 2009-01-20T20:15:07Z
dc.date.issued 2008-06-26
dc.description This presentation was part of the session : Cross Cutting Technologies en_US
dc.description Sixth International Planetary Probe Workshop en_US
dc.description.abstract Mars Gravity Biosatellite is a novel program aimed at providing data on the effects of partial gravity on mammalian physiology. A collaboration between MIT and Georgia Tech, this student-developed free-flyer spacecraft is designed to carry a payload of 15 mice into low Earth orbit, rotating to generate accelerations equivalent to Martian gravity. After 35 days, the payload will re-enter the atmosphere and be recovered for study. Having engaged more than 500 students to date in space life science, systems engineering, and hardware development, the Mars Gravity Biosatellite program offers a unique, interdisciplinary educational opportunity to address a critical challenge in the next steps in human space exploration through the development of a free-flyer platform for partial gravity science with full entry, descent, and landing (EDL) capability. Execution of a full entry, descent, and landing from low Earth orbit is a rare requirement among university-class spacecraft. The EDL design for the Mars Gravity Biosatellite is driven by requirements on the allowable deceleration profile for a payload of de-conditioned mice and maximum allowable recovery time. The 260 kg entry vehicle follows a ballistic trajectory from low Earth orbit to a target recovery site at the Utah Test and Training Range. Reflecting an emphasis on design simplicity and the use of heritage technology, the entry vehicle uses the Discoverer aeroshell geometry and leverages aerodynamic decelerators for mid-air recovery and operations originally developed for the Genesis mission. This paper presents the student-developed EDL design for the Mars Gravity Biosatellite, with emphasis on trajectory design, dispersion analysis, and mechanical design and performance analysis of the thermal protection and parachute systems. Also included is discussion on EDL event sequencing and triggers, contingency operations, the deorbit of the spacecraft bus, plans for further work, and the educational impact of the Mars Gravity Biosatellite program. en_US
dc.identifier.uri http://hdl.handle.net/1853/26430
dc.publisher Georgia Institute of Technology en_US
dc.relation.ispartofseries IPPW08. Cross Cutting Technologies en_US
dc.subject Entry, Descent, and Landing (EDL) en_US
dc.subject Student spacecraft en_US
dc.subject Partial gravity en_US
dc.title Entry, Descent, and Landing System Design for the Mars Gravity Biosatellite en_US
dc.type Text
dc.type.genre Proceedings
dspace.entity.type Publication
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.contributor.corporatename College of Engineering
local.relation.ispartofseries International Planetary Probe Workshop (IPPW)
relation.isOrgUnitOfPublication a348b767-ea7e-4789-af1f-1f1d5925fb65
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
relation.isSeriesOfPublication 6369d36f-9ab2-422f-a97e-4844b98f173b
Original bundle
Now showing 1 - 2 of 2
Thumbnail Image
4.56 MB
Adobe Portable Document Format
Thumbnail Image
7.64 MB
Adobe Portable Document Format
PDF Presentation