HALCA's onboard VLBI observing system

被引:12
|
作者
Kobayashi, H
Wajima, K
Hirabayashi, H
Murata, Y
Kawaguchi, N
Kameno, S
Shibata, KM
Fujisawa, K
Inoue, M
Hirosawa, H
机构
[1] Natl Astron Observ, Tokyo 1818588, Japan
[2] Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2298510, Japan
关键词
space vehicles : instruments techniques : interferometric;
D O I
10.1093/pasj/52.6.967
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The first space VLBI satellite, HALCA, was launched on 1997 February 12. We report the characteristics of HALCA as an orbiting VLBI station with 8-m deployment antenna. It is required the high system gain, low system noise, and high stability of phase transfer. And the stabilities of system gain and system noise are needed for imaging of VLBI. HALCA achieved the requirement as a VLBI stations and has made almost 3 times longer baselines than ground global VLBI networks. It means observations with 3 times higher angular resolution have been carried out. We have measured aperture efficiencies of the deployment antenna, system noise temperatures, stability of onboard local oscillators, and stability of phase link. HALCA's onboard radio astronomy system has 1.60-1.73 GHz, 4.7-5.0 GHz, and 21.9-22.3 GHz receivers and two-channel high-rate samplers. Typical values of system noise temperature in orbit are 70 K and 90 K at 1.6 and 5 GHz respectively. At 22 GHz, the apparent system noise temperature is 400 K; however, this is mostly due to attenuation between the main antenna and the 22 GHz low noise amplifier. A reference tone signal is transmitted from a ground tracking station which is locked on a ground hydrogen maser oscillator. The internal phase stability of local oscillators is around 5 degrees r.m.s. at 5 GHz. The total gain of the receiving system and the bit distribution of the high-rate samplers have also been checked. With the exception of the 22 GHz attenuation, the in-orbit performance of the VLBI observing system matches the ground-test results very well.
引用
收藏
页码:967 / 973
页数:7
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