A Q-switched laser system was applied to a research rocket combustor in order to ignite cryogenic propellants by inducing several plasma breakdown events. The optical emission was analyzed using LIBS and other techniques.

© 2019 The Author(s)

PDF Article


You do not have subscription access to this journal. Citation lists with outbound citation links are available to subscribers only. You may subscribe either as an OSA member, or as an authorized user of your institution.

Contact your librarian or system administrator
Login to access OSA Member Subscription