Requirements and design structure for Surya Satellite-1

4th International Symposium on LAPAN-IPB Satellite for Food Security and Environmental Monitoring

农业科学;生态环境科学

Steven, H.^1 ; Huzain, M.F.^2

Engineering Physics Department, Surya University, Banten, Tangerang

15810, Indonesia^1

National Institute of Aeronautics and Space, Centre of Satellite Technology, West Java, Bogor

16310, Indonesia^2

关键词: Anodizations;    Anodized aluminum;    Center points;    Design structure;    Interface control documents;    Japan Aerospace Exploration Agency;    Manufacturing process;    Satellite structure;   

Others  :  https://iopscience.iop.org/article/10.1088/1755-1315/149/1/012063/pdf
DOI  :  10.1088/1755-1315/149/1/012063

来源: IOP

【 摘 要 】

Currently, there are various references on the manufacture of nanosatellite specifications weighing 1KG - 10KG.The Surya Satellite-1 is the first nanosatellite made by universities in Indonesia. The Surya Satellite-1 team gets a launch offer from Japan Aerospace Exploration Agency (JAXA) and, all the nanosatellites manufacturer racers at ICD (Interface Control Document) obtained from JAXA. The formation of the Satellite-1 Surya framework is also based on the provisions of JAXA. The various specifications and requirements specified by the JAXA space agency consisting of specific specifications such as the mass of nanosatellite 1U (10cm x 10cm x 11.65cm) size of at least 0.13KG and a maximum of 1.33KG, with the determination of a gravity point not exceeding 2 cm from the nanosatellite geometry center point. In the case of preventing solar radiation in space, there is a requirement that the structure of satellite structures on hard black anodization should be more than 10 meters in the surface of the satellite structure. In terms of detail, the satellite structure is a black hard anodized aluminum after its manufacturing process derived from the MIL-A-8625 document, type 3.