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  5. Atmospheric Entry Performance of the Hercules Single-Stage Reusable Vehicle at Earth
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Atmospheric Entry Performance of the Hercules Single-Stage Reusable Vehicle at Earth

Date Issued
December 15, 2019
Author(s)
Brakefield, Braxton Lott
Advisor(s)
James Evans Lyne
Additional Advisor(s)
Zhili Zhang
John Schmisseur
Permanent URI
https://trace.tennessee.edu/handle/20.500.14382/41772
Abstract

The Hercules Single-Stage Reusable Vehicle (HSRV) is an innovative rocket that has been designed for use at Mars. However, with the renewed focus on returning to the moon first, it has been proposed to use the Hercules design for missions in the Earth-Moon system. To test its reentry performance, 9 types of entries were simulated, with multiple sensitivity cases for each. Overall, the current design of the vehicle is able to return to Earth safely for a wide range of different entry conditions, but some improvements could be made to optimize the vehicle for Earth operations.

Subjects

Reentry

Hercules

HSRV

Atmospheric Entry

Spaceflight

Aerocapture

Degree
Master of Science
Major
Aerospace Engineering
File(s)
Thumbnail Image
Name

utkirtd_12831.pdf

Size

4.6 MB

Format

Adobe PDF

Checksum (MD5)

d94643411a888cee60c77c914d95f79c


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