CubeSat Laser Infrared CrosslinK

Mayer, David J ; Fishman, Julianna L ; Cahoy, Kerri

关键词: CROSSLINKING;    CUBESATS;    DISTANCE;    INFRARED LASERS;    LOW EARTH ORBITS;    MEASURING INSTRUMENTS;    OPTICAL COMMUNICATION;    POINTING CONTROL SYSTEMS;    POSITION (LOCATION);    RATES (PER TIME);    RISK;    SPACECRAFT ORBITS;   

RP-ID  :  ARC-E-DAA-TN67946

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The CubeSat Laser Infrared CrosslinK (CLICK) mission will demonstrate technology to advance the state of the art in communications between small spacecraft as well as the capability to gauge their relative distance and location. CLICK is comprised of two sequential missions. The first mission, CLICK A, is a risk reduction mission that will test out elements of the optical (laser) communications with a single 3-unit (3U) spacecraft. The key objective of this risk reduction testing is to demonstrate the fine steering mirror control system's high precision pointing performance which enables the use of a lower power laser in CLICK B/C. The goal of CLICK B/C, the second mission, is to demonstrate full-duplex (send and receive) optical communication crosslink between two 3U small spacecraft, in low-Earth-orbit, at distances between 15 and 360 miles (25 - 580 kilometres) apart at data rates greater than 20 Mbps.