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/10.1088/1742-6596/1005/1/012044Additional details
Identifiers
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