Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Olive R. Stohlman"'
Autor:
Miria M. Finckenor, Randall Barfield, Olive R. Stohlman, W. Keats Wilkie, Benjamin R. Sindle, Amanda E. Stark, Robert G. Bryant, Jin Ho Kang, Keith L. Gordon, Paul D. Craven
Publikováno v:
Advances in Space Research. 67:2643-2654
The construction of a solar sail from commercially available metallized film presents several challenges. The solar sail membrane is made by seaming together precut lengths of ultrathin metallized polymer film into the required geometry. This assembl
Publikováno v:
Astrodynamics, 3(3)
This paper proposes the use of solar-sail technology currently under development at NASA Langley Research Center for a CubeSat rendezvous mission with asteroid 2016 HO3, a quasi-satellite of Earth. Time-optimal trajectories are sought for within a 20
Autor:
Juan M. Fernandez, Jerry E. Warren, M.J. Heiligers, Olive R. Stohlman, Jin Ho Kang, Nigel R. Schneider, Gregory D. Dean, W. Keats Wilkie, Sarah M. Cook
Publikováno v:
AIAA Scitech 2021 Forum.
An overview of the NASA Advanced Composite Solar Sail System (ACS3) technology demonstration project is presented. Descriptions of the ACS3 solar sail design, spacecraft systems, concept of operations, and ground testing are provided, along with a di
Publikováno v:
AIAA Scitech 2021 Forum.
Autor:
Gregory D. Dean, Juan M. Fernandez, Olive R. Stohlman, Randall Barfield, Jin Ho Kang, Taylor J. Herndon, Nigel R. Schneider, Peter Stokes
Publikováno v:
AIAA Scitech 2020 Forum.
Solar sail membranes must have a high area-to-mass ratio and high solid volume fraction when stowed. In order to meet mission requirements, current solar sail projects, such as NASA’s Near Earth Asteroid Scout, require metallized sail membranes wit
Autor:
Olive R. Stohlman, Nigel R. Schneider, Juan M. Fernandez, Gregory D. Dean, Randall Barfield, Jin Ho Kang, Taylor J. Herndon, Peter Stokes
Publikováno v:
AIAA Scitech 2019 Forum.
Autor:
Olive R. Stohlman
Publikováno v:
2018 AIAA Spacecraft Structures Conference.
Autor:
Keats W. Wilkie, Juan M. Fernandez, Jerry E. Warren, Gregory D. Dean, Olive R. Stohlman, Casey J. Younger, Jin Ho Kang, Robert G. Bryant, Geoff Rose
Publikováno v:
2018 AIAA Spacecraft Structures Conference.
Autor:
Guglielmo S. Aglietti, Mark Schenk, Sven Erb, Olive R. Stohlman, Lourens Visagie, Vaios Lappas, Juan M. Fernandez
Publikováno v:
Acta Astronautica. 103:204-225
The accumulation of space debris in low Earth orbits poses an increasing threat of collisions and damage to spacecraft. As a low-cost solution to the space debris problem the Gossamer Deorbiter proposed herein is designed as a scalable stand-alone sy
Autor:
Olive R. Stohlman, Erik R. Loper
Publikováno v:
3rd AIAA Spacecraft Structures Conference.
Metallic triangular rollable and collapsible (TRAC) booms have deployed two Cubesatbased solar sails in low Earth orbit, making TRAC booms the most popular solar sail deployment method in practice. This paper presents some concerns and solutions surr