Jump to content
Main menu
Main menu
move to sidebar
hide
Navigation
Main page
Recent changes
Random page
Help about MediaWiki
Special pages
Niidae Wiki
Search
Search
Appearance
Create account
Log in
Personal tools
Create account
Log in
Pages for logged out editors
learn more
Contributions
Talk
Editing
Beam-powered propulsion
(section)
Page
Discussion
English
Read
Edit
View history
Tools
Tools
move to sidebar
hide
Actions
Read
Edit
View history
General
What links here
Related changes
Page information
Appearance
move to sidebar
hide
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
===Laser thermal rocket=== {{Main|Thermal rocket}} A laser thermal rocket is a [[thermal rocket]] in which the propellant is heated by energy provided by an external laser beam.<ref>H. Krier and R. J. Glumb. [http://arc.aiaa.org/doi/abs/10.2514/3.8610 "Concepts and status of laser-supported rocket propulsion"], ''Journal of Spacecraft and Rockets'', Vol. 21, No. 1 (1984), pp. 70-79. https://dx.doi.org/10.2514/3.8610</ref><ref>{{cite book | chapter-url=http://arc.aiaa.org/doi/abs/10.2514/5.9781600865633.0129.0148 | doi=10.2514/5.9781600865633.0129.0148 | chapter=Laser Thermal Propulsion | title=Orbit-Raising and Maneuvering Propulsion: Research Status and Needs | year=1984 | pages=129β148 | isbn=978-0-915928-82-8 }}</ref> In 1992, the late [[Jordin Kare]] proposed a simpler, nearer-term concept with a rocket containing liquid hydrogen.<ref>Kare, J. T. (1992). Development of Laser-Driven Heat Exchanger Rocket for Ground to-Orbit Launch. Washington, DC International Astronautical Federation Congress. {{bibcode|1992wadc.iafcQY...K}}</ref> The propellant is heated in a heat exchanger that the laser beam shines on before leaving the vehicle via a conventional nozzle. This concept can use continuous beam lasers, and the semiconductor lasers are now cost-effective for this application.<ref>{{cite web | url=http://www.niac.usra.edu/files/library/meetings/fellows/mar04/897Kare.pdf |archive-url=https://ghostarchive.org/archive/20221009/http://www.niac.usra.edu/files/library/meetings/fellows/mar04/897Kare.pdf |archive-date=2022-10-09 |url-status=live | title=Modular Laser Launch Architecture: Analysis and Beam Module Design | work=niac.usra.edu | date=March 24, 2004 | access-date=July 19, 2016 | author=Jordin T. Kare}}</ref><ref>{{cite web|url=http://www.jkare.com/VG_HX_4-29-SAS.pdf |access-date=August 11, 2010 |url-status=dead |archive-url=https://web.archive.org/web/20110724205642/http://www.jkare.com/VG_HX_4-29-SAS.pdf |archive-date=July 24, 2011|title=HX Laser Launch: It's Steamship Time}}</ref>
Summary:
Please note that all contributions to Niidae Wiki may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see
Encyclopedia:Copyrights
for details).
Do not submit copyrighted work without permission!
Cancel
Editing help
(opens in new window)
Search
Search
Editing
Beam-powered propulsion
(section)
Add topic