作者: Brian Hicks
DOI: 10.1007/978-1-4614-8211-6_5
关键词:
摘要: A large number of designs for space-based high-contrast coronagraphy-enabled Explorers have been laboratory proven and proposed. Their complexity costliness along with a need to raise the Technological Readiness Level (TRL) many key components concepts kept most at breadboard stage development, however. In this chapter I provide detailed comparison two nulling techniques that used in instrumentation designed built operation, one which has flown.