Published April 1, 2018 | Version v1
Journal article

Preliminary Design of Nano Satellite for Regional Navigation System

  • 1. Faculty of Mechanical and Aerospace Engineering, Institut Teknologi Bandung (Indonesia)

Description

A Low cost Regional Navigation Satellite System employing constellation of nano satellites has been proposed for Indonesian coverage. The constellation of Low Earth Orbit nano satellites off course will not be able to give better position fixed to the GPS. However, the design of navigation system has much lower in cost compare to the current navigation system. This paper tells about preliminary design of the proposed regional navigation satellite system. The results of our satellite design has 3 kg on its weight, 10 W on power requirement at the peak condition, and 2.7 years of lifetime. Payload communication of the satellite will use UHF and TT&C communication will use VHF. Total area of solar panel will be 0.11 m2. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1742-6596/1005/1/012044

Additional details

Publishing Information

Journal Title
Journal of Physics. Conference Series (Online)
Journal Volume
1005
Journal Issue
1
Journal Page Range
[9 p.]
ISSN
1742-6596

Conference

Title
5. International Seminar on Aerospace Science and Technology
Dates
27-29 Sep 2017
Place
Medan (Indonesia)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52090270
Subject category
S79: ASTROPHYSICS, COSMOLOGY AND ASTRONOMY; S46: INSTRUMENTATION RELATED TO NUCLEAR SCIENCE AND TECHNOLOGY; S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
GLOBAL POSITIONING SYSTEM; NAVIGATION; ORBITS; SATELLITES; WEIGHT