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• W175047105 abstract "ARAPAIMA is a proximity operations mission sponsored by the US Air Force Office of Scientific Research (AFOSR) and the Air Force Research Laboratory (AFRL), to perform the in-orbit demonstration of autonomous proximity operations for visible, infrared, and point cloud generation of resident space objects (RSOs) from a nanosat platform. The nanosat is of the 6U CubeSat class, with overall dimensions of 12x24x36cm, a mass of 9.78kg, and has been selected as part of AFRL’s University NanoSat Program (UNP) Cycle 8. This paper describes the mission goals, concept of operations, science objectives and subsystem design and selection, with focus given to a detailed mission analysis and the requirements flow-down. By demonstrating robust, affordable, and responsive rendezvous and proximity operations of a nanosat with an uncooperative RSO, successful completion of the ARAPAIMA mission will validate a range of technologies for space-based space 12situational awareness (SSA) and debris removal from Low Earth Orbit (LEO).In addition, the mission will validate a set of key technologies and their integration at system level, such as miniaturized commercially available sensors, a miniaturized warm gas propulsion system for CubeSat applications, as well as advanced relative navigation and proximity operations algorithms implemented on a nanosat. MISSION OPERATIONS CONCEPT/OVERVIEW ARAPAIMA stands for “Application for RSO Autonomous Proximity Analysis and IMAging”. ARAPAIMA is a proximity operations mission sponsored by the US Air Force Office of Scientific Research (AFOSR) and the Air Force Research Laboratory (AFRL), through the University Nanosat Program, to perform the in-orbit demonstration of autonomous proximity operations for visible, infrared, and three dimensional imaging of resident space objects (RSOs) on a cubesat platform. The payload consists of a commercially available infrared (IR) camera and a miniature laser rangefinder (LRF) with a range of a few km. The instruments are installed on the cubesat so that their optical axes are pointing in the same direction. The cubesat is equipped with a warm gas propulsion system which enables it to perform orbital maneuvering and reaction control of attitude. The goal of the ARAPAIMA mission is to perform the in-orbit demonstration of autonomous proximity operations for visible, infrared, and three dimensional imaging of RSOs. ARAPAIMA is of the 6U cubesat class with overall dimensions of 12x24x36cm. The ARAPAIMA cubesat can be seen in Figure 1. Figure 1: CAD model of the ARAPAIMA Cubesat Mission Concept of Operations The in-orbit operations of ARAPAIMA and specific proximity operation scenarios can be broken down into five steps. Each of the five mission steps is tied-in with" @default.
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• W175047105 date "2013-08-05" @default.
• W175047105 modified "2023-09-27" @default.
• W175047105 title "Application for RSO Automated Proximity Analysis and IMAging (ARAPAJMA): Development of a Nanosat-based Space Situational Awareness Mission" @default.
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