NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Preliminary Coating Development for Solar Thermal Propulsion (STP)Solar Thermal Propulsion (STP) utilizes the sun’s thermal energy to create thrust, enabling rapid transit to interstellar medium via the Oberth Maneuver. For this, the system would fly very close to the sun, so an optical, “white” coating on a graphite substance is required to regulate the system’s temperature. However, standard heat shield coatings degrade over the STP heating profile of 2500 °K over multiple hours. Thus, an optical coating should be designed with the ability to control reflectance and microstructural evolution during operation.
Document ID
20230011584
Acquisition Source
Ames Research Center
Document Type
Poster
Authors
Sander L. Bouchard
(Colorado School of Mines Golden, Colorado, United States)
William T. Burke
(University of Vermont Burlington, Vermont, United States)
Peter Edward Marshall
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Brody Kelly Bessire
(Ames Research Center Mountain View, California, United States)
Date Acquired
August 4, 2023
Subject Category
Solar Physics
Meeting Information
Meeting: OTESM Poster Session
Location: San Francisco, CA
Country: US
Start Date: August 9, 2023
Sponsors: OSTEM
Funding Number(s)
WBS: 335803.04.22.21.10.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Solar Thermal Propulsion
Coating
Thermal Protection System
No Preview Available