Title :
Spacecraft-level verification of the Van Allen Probes´ RF communication system
Author :
Crowne, Matthew J. ; Srinivasan, Dipti ; Royster, D. ; Weaver, G. ; Matlin, D. ; Mosavi, N.
Author_Institution :
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
Abstract :
This paper presents the verification process, lessons learned, and selected test results of the radio frequency (RF) communication system of the Van Allen Probes, formerly known as the Radiation Belt Storm Probes (RBSP). The Van Allen Probes mission is investigating the doughnut-shaped regions of space known as the Van Allen radiation belts where the Sun interacts with charged particles trapped in Earth´s magnetic field. Understanding this dynamic area that surrounds our planet is important to improving our ability to design spacecraft and missions for reliability and astronaut safety. The Van Allen Probes mission features two nearly identical spacecraft designed, built, and operated by the Johns Hopkins University Applied Physics Laboratory (JHU/APL) for the National Aeronautics and Space Administration (NASA). The RF communication system features the JHU/APL Frontier Radio. The Frontier Radio is a software-defined radio (SDR) designed for spaceborne communications, navigation, radio science, and sensor applications. This mission marks the first spaceflight usage of the Frontier Radio. RF ground support equipment (RF GSE) was developed using a ground station receiver similar to what will be used in flight and whose capabilities provided clarity into RF system performance that was previously not obtained until compatibility testing with the ground segments. The Van Allen Probes underwent EMC, acoustic, vibration, and thermal vacuum testing at the environmental test facilities at APL. During this time the RF communication system was rigorously tested to ensure optimal performance, including system-level testing down to threshold power levels. Compatibility tests were performed with the JHU/APL Satellite Communication Facility (SCF), the Universal Space Network (USN), and the Tracking and Data Relay Satellite System (TDRSS). Successful completion of this program as described in this paper validated the design of the system and demonstrated that it will be able to me- t all of the Van Allen Probes´s communications requirements with its intended ground segments.
Keywords :
Sun; aircraft communication; aircraft navigation; geomagnetism; radiation belts; relay networks (telecommunication); reliability; satellite communication; satellite tracking; software radio; Applied Physics Laboratory; EMC; Earth magnetic field; JHU/APL Satellite Communication Facility; Johns Hopkins University; NASA; National Aeronautics and Space Administration; RBSP; RF GSE; RF ground support equipment; Radiation Belt Storm Probes; SDR; Sun; TDRSS; USN; Universal Space Network; Van Allen radiation belts; astronaut safety; data relay satellite system; doughnut-shaped regions; ground station receiver; navigation; radio frequency communication; radio science; reliability; software-defined radio; spaceborne communications; spacecraft-level verification; spaceflight usage; tracking relay satellite system; verification process; Downlink; Orbits; Probes; Radio frequency; Space vehicles; Testing; Uplink;
Conference_Titel :
Aerospace Conference, 2013 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4673-1812-9
DOI :
10.1109/AERO.2013.6497149