Antenna coupled kinetic inductance detectors for space based sub-mm astronomy
                                            conference paper
                                        
                                    
                                            To achieve background limited detection, future space missions in the far infrared and sub-mm radiation bands will require
large arrays (>1000 pixels) of very sensitive detectors. A typical requirement for the noise equivalent power is 10^-19
W/Hz^0.5 for a Fourier Transform Spectrometer, which is 100 to 1000 times more sensitive than the state of the art such as on
HERSCHEL. Such low NEP is a significant technical challenge, both to achieve for the detectors and to demonstrate in the
laboratory. Kinetic inductance detectors can theoretically achieve this performance and have significant advantages over other
types of detectors, for example are well adapted to frequency domain multiplexing. We present antenna coupled kinetic
inductance detectors, showing the loaded optical NEP measured with a well controlled narrow band black body radiation
source. We will also discuss the optimization route required to reach the requirements for future missions, including the
optical testing requirements
                                    large arrays (>1000 pixels) of very sensitive detectors. A typical requirement for the noise equivalent power is 10^-19
W/Hz^0.5 for a Fourier Transform Spectrometer, which is 100 to 1000 times more sensitive than the state of the art such as on
HERSCHEL. Such low NEP is a significant technical challenge, both to achieve for the detectors and to demonstrate in the
laboratory. Kinetic inductance detectors can theoretically achieve this performance and have significant advantages over other
types of detectors, for example are well adapted to frequency domain multiplexing. We present antenna coupled kinetic
inductance detectors, showing the loaded optical NEP measured with a well controlled narrow band black body radiation
source. We will also discuss the optimization route required to reach the requirements for future missions, including the
optical testing requirements
TNO Identifier
                                        
                                            484266
                                        
                                    Source title
                                        
                                            19th International Symposium on Space Terahertz Technology, ISSTT 2008, 28-30 April 2008, Groningen, Netherlands
                                        
                                    Pages
                                        
                                            121