• Title/Summary/Keyword: Orbiter compressor

Search Result 3, Processing Time 0.015 seconds

Performance Analysis of an Orbiter Air Compressor (오비터 공기 압축기 성능해석)

  • Kim, Hyun-Jin;Cho, Kwang-Myoung;Ko, Won
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
    • /
    • v.17 no.8
    • /
    • pp.754-763
    • /
    • 2005
  • This paper introduces a new concept compressor in which piston orbits in the cylinder having an annular space formed between two concentric circular walls. In this configuration, two gas pockets are formed with $180^{\circ}$ phase difference: one between the wrap of the orbiting piston and the inner cylinder wall and the other between the piston wrap and the outer cylinder wall. This alternating feature of gas compression and discharge processes yields several advantages such as low torque variation and low gas pulsation. Computer simulation program has been developed to evaluate the compressor performance. The volumetric, adiabatic, and mechanical efficiencies of the orbiter compressor are calculated to be $85.6\%,\;97.2\%,\;and\;95.2\%$, respectively, when it is used as an air compressor.

Development of Kinematic Ephemeris Generator for Korea Pathfinder Lunar Orbiter (KPLO)

  • Song, Min-Sup;Park, Sang-Young;Kim, Youngkwang;Yim, Jo Ryeong
    • Journal of Astronomy and Space Sciences
    • /
    • v.37 no.3
    • /
    • pp.199-208
    • /
    • 2020
  • This paper presents a kinematic ephemeris generator for Korea Pathfinder Lunar Orbiter (KPLO) and its performance test results. The kinematic ephemeris generator consists of a ground ephemeris compressor and an onboard ephemeris calculator. The ground ephemeris compressor has to compress desired orbit propagation data by using an interpolation method in a ground system. The onboard ephemeris calculator can generate spacecraft ephemeris and the Sun/Moon ephemeris in onboard computer of the KPLO. Among many interpolation methods, polynomial interpolation with uniform node, Chebyshev interpolation, Hermite interpolation are tested for their performances. As a result of the test, it is shown that all the methods have some cases that meet requirements but there are some performance differences. It is also confirmed that, the Chebyshev interpolation shows better performance than other methods for spacecraft ephemeris generation, and the polynomial interpolation with uniform nodes yields good performance for the Sun/Moon ephemeris generation. Based on these results, a Kinematic ephemeris generator is developed for the KPLO mission. Then, the developed ephemeris generator can find an approximating function using interpolation method considering the size and accuracy of the data to be transmitted.