DocumentCode :
2267955
Title :
Constella, a quick configuration platform for rapid response missions
Author :
Meerman, Maarten ; Sweeting, Martin
Author_Institution :
Surrey Satellite Technol. Ltd., Surrey Univ., Guildford
fYear :
0
fDate :
0-0 0
Abstract :
Constella is a novel very quick response satellite platform that can be used in any low Earth orbit. It can be used as a single unit or as part of a constellation of spacecraft. It can be pre-manufactured to a large extent, and a selection of subsystems can be ready to select from, to provide last-minute configuration options for both the payload and platform. This satellite contains a number of innovations that have not been used in space before, and they will allow very quick response missions to take place. Only a very short time is required to decide on the mission and plan the satellite design, then assemble the final parts, and test and launch the satellite into orbit. The total time can be down to weeks or even days. Unlike most quick-response missions, where anything under one year is included, and where the satellite typically has to be completely ready and tested, waiting for quick call-up, the Constella can be tailored with interchangeable attitude sensors, propulsion units, communications equipment, payloads and more, just before launch, even right at the launch site if required. The platform produces almost the same amount electrical power, irrespective of orbital inclination or ascending node time, removing the need for solar panel design changes at the configuration stage. Additionally, the design of the platform allows for optimized initial manufacture, requiring very little assembly and integration space and time, in itself a major cost saver. The paper discusses the specific technical aspects of the design of the platform, showing the innovations that are both physical and operational. It shows proposed missions that can take advantage of this platform, allowing them to proceed where traditional rapid response or low cost engineering techniques will not be feasible
Keywords :
artificial satellites; satellite communication; space research; Constella; ascending node time; attitude sensors; communications equipment; electrical power; low Earth orbit; orbital inclination; propulsion units; rapid response missions; satellite platform; solar panel design; spacecraft constellation; Artificial satellites; Assembly; Communication equipment; Low earth orbit satellites; Payloads; Propulsion; Space missions; Space vehicles; Technological innovation; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2006 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-9545-X
Type :
conf
DOI :
10.1109/AERO.2006.1655830
Filename :
1655830
Link To Document :
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