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Cryogenic performance of the SIRTF prototype secondary mirror assembly

机译:SIRTF原型二手镜组件的低温性能

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The Space Infrared Telescope Facility (SIRTF), planned for an early 21st century launch into a 100,000 km orbit, will be the fourth of NASA's great observatories. It contains a 1-meter class Ritchey-Chretien telescope, all the components of which will be cryogenically cooled to superfluid helium temperatures. Efficient use of SIRTF's limited cryogenic lifetime (5 years, with a sensitivity of approximately 0.5 month/mW) requires a very low power means for tilting the secondary mirror to relocate rapidly the telescope's line of sight and to map small regions of the sky. Furthermore, at the longest SIRTF wavelengths (200 - 1200 $mu@m) the emission from the cooled telescope will be significant, thereby requiring the use of periodic tilt oscillations of the secondary mirror to modulate the astronomical signal. In addition, achievement of diffraction-limited performance at wavelengths as short as 3 $mu@m will require realignment of the secondary mirror following cool-down and launch. The technology for achieving the secondary mirror assembly requirements at liquid helium temperatures with space-qualifiable hardware had not been developed at the inception of the prototype secondary mirror assembly (PSMA) program in January 1988. We describe in this paper the results of the first liquid helium temperature testing of the SIRTF PSMA. In addition to providing the conventional functions of telescope focus (0.8 $mu@m secondary mirror resolution) and collimation adjustment, the PSMA must achieve 0.063 $mu@m rms wavefront error and millikelvin/sec mirror thermal stability at about 2 K while providing the functions of stable two-axis pointing (0.15 arcsec rms secondary mirror jitter) and dc and dynamic tilting (`chopping,' up to $POM 14 arcmin at 5 Hz) with square, sawtooth, and triangle waveforms. The cryogenic power dissipation budget is 5 mW. We present liquid helium temperature measurements of the PSMA tilt jitter, drift, and range, the reaction mass dynamics, cryogenic power dissipation, and mirror thermal stability. The initial tests of the PSMA strongly indicate that the SIRTF requirements can indeed be met.
机译:空间红外望远镜设施(SIRTF),计划在21世纪初推出到10万公里的轨道,将成为第四美国宇航局的大天文台的。它包含1米类里奇 - 克莱琴望远镜,所有这些组件将被低温冷却至超流体氦的温度。有效地利用SIRTF的限制低温寿命(5年,约0.5个月/毫瓦的灵敏度)需要一个非常低的功率装置,用于倾斜所述次镜迅速重新定位的视线望远镜的线和天空的小区域进行映射。此外,在最长波长SIRTF(200 - 1200 $亩@米)从冷却的望远镜的发射将是显著,从而需要使用的副镜的周期性倾斜振荡来调制天文信号。此外,在波长越短3 $亩衍射极限性能成就@米将需要下面的冷却和推出的次镜的调整。为实现在液氦温度与空间qualifiable硬件辅助镜组件需求的技术还没有在原型二次反射镜组件(PSMA)计划于1988年一月以来我们描述了在本文中被开发的第一液体的结果氦温度SIRTF PSMA的测试。除了提供望远镜焦点的常规功能(0.8 $亩@ M个次级镜分辨率)和准直调整,PSMA必须在约2千达到0.063 $亩@米均方根波前误差和毫开尔文/秒镜的热稳定性,同时提供稳定两轴指向(0.15弧秒均方根副镜抖动)和dc和动态倾斜的功能('斩波”高达$ POM 14在5Hz弧分)具有正方形,锯齿和三角形波形。低温功耗预算为5毫瓦。我们的PSMA倾斜抖动,漂移和范围,将反应物料动力学,低温功耗的本发明的液体氦的温度测量,和反射镜的热稳定性。在PSMA的初步测试强烈表明,SIRTF要求确实可以得到满足。

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