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Development of a Transportable Telescope for Galactic Survey at 500 GHz in Antarctica

机译:在南极洲开发用于500 GHz银河测量的便携式望远镜

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We have developed a transportable 30-cm submillimeter-wave telescope to operate at the Dome Fuji station in the Antarctic plateau. Transportability is an important requirement in the design; the telescope can be divided into several subsystems by hands. The maximum weight of the subsystems is restricted to be below 60 kg, so that the telescope can be assembled without a lifting machine. A small 4 K mechanical cryocooler is used for cooling down a SIS mixer. Total power consumption was designed to be less than 2.5 kW. The optical system was designed to satisfy the frequency independent matching condition at the subreflector and the feed horn of the SIS mixer, so we could accommodate a higher frequency receiver without changing mirrors. A quasi-optical filter was employed for the single sideband operation in observations of the CO (J = 4-3) line at 461.04 GHz and the [CI] (3P1-3P0) line at 492.16 GHz. It was equipped with a 1 GHz width spectrometer that covers a velocity width of 600 km/s with a velocity resolution of 0.04 km/s at 461 GHz. We carried out test observations at a 4400-m altitude site in northern Chile during winters of 2010 and 2011. The typical system noise temperature, including atmospheric loss, was 3000 K (SSB) at 461 GHz, that is mainly limited by atmospheric opacity. The beam size of the 30-cm offset Cassegrain antenna at 0.65 mm of wavelength was measured to be 9'.4±0'.4 by cross scanning of the sun. This angular resolution of the 30-cm telescope is same as those of the Columbia-CfA-U. Chile CO (J = 1-0) surveys. We estimated the main beam efficiency to be 87±5% by observing the new moon. We succeeded in mapping Orion Molecular Cloud A and M17 SW in CO (J = 4-3) followed by test observations toward Orion KL in both CO (J = 4-3) and [CI] (3P1-3P0) .
机译:我们已经开发了一种可移动的30厘米亚毫米波望远镜,可以在南极高原的巨蛋富士站工作。可运输性是设计中的重要要求。人工将望远镜分为几个子系统。子系统的最大重量限制在60千克以下,因此可以在不使用提升机的情况下组装望远镜。小型4 K机械低温冷却器用于冷却SIS混合器。总功耗被设计为小于2.5 kW。光学系统的设计满足了SIS混频器的子反射器和馈入喇叭处与频率无关的匹配条件,因此我们可以容纳更高频率的接收器而无需更换反射镜。在461.04 GHz的CO( J = 4-3)线和[CI]( 3 < i> P 1 - 3 P 0 )线,频率为492.16 GHz。它配备了一个1 GHz宽度的光谱仪,该光谱仪的速度宽度为600 km / s,在461 GHz时的速度分辨率为0.04 km / s。我们在2010年和2011年冬季在智利北部4400米高空进行了测试观察。在461 GHz频率下,典型的系统噪声温度(包括大气损耗)为3000 K(SSB),这主要受大气不透明度的限制。通过太阳的交叉扫描,在0.65 mm波长处的30 cm偏置卡塞格伦天线的波束尺寸为9'.4±0'.4。 30厘米望远镜的角分辨率与Columbia-CfA-U的角分辨率相同。智利CO( J = 1-0)调查。通过观察新月,我们估计主光束效率为87±5%。我们成功地绘制了CO中的Orion分子云A和M17 SW( J = 4-3),然后对两个CO( J = 4-3)中的Orion KL进行了测试观察)和[CI]( 3 P 1 - 3 P 0 )。

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