CSO History

THE DISH

Back ] Up ] Next ]


A

 s Robert Leighton turned his attention to devising methods for making larger (~10m)   telescopes for millimeter wavelengths, his particular concern was how to create a   large but light-weight reflecting surface which would maintain its parabolic figure when pointing from horizon to zenith, or when impacted by wind. Initially, he tried spinning an epoxy coated surface , but was thwarted by ripples which developed in the epoxy. He then came up with a brilliant design, characterized by hexagonal, lightweight aluminum honeycomb panels, supported by a steel tube back-up structure. The steel tubes were used to construct a strut and post array, based on a lattice of equilateral triangles that could hold the surface of the dish in the proper shape. He developed a very simple BASIC computer program to calculate the lengths of the various struts and posts. It turned out that in order to maintain the surface shape to the desired tolerances, the length of each element had to be accurate to less than three thousandths of an inch, so that a laser interferometer was required to construct the elements to the correct lengths.

Figure 1. Robert Leighton in the 1960s

This design showed so much promise that it caught the imagination of the director of OVRO, Al Moffet, a Caltech professor of radio astronomy and an expert in interferometry techniques. Together with Neugebauer and Leighton, he proposed to the NSF to build three antennas as a millimeter-wave interferometer in the Owens Valley, together with a fourth, more accurate version, to be sited on a high mountain.

The basic idea behind this back-up structure was that an array of posts parallel to each other and to the optic axis would support the reflecting surface in the correct shape if they were held together in a rigid structure with struts [1][2]. The struts had to be attached to the posts in such a way that the axes of the struts, connected to an end of a post, had to all pass through the same point along the axis of the post. In this way there would be no net twisting or bending force on a post. Struts from the ends of each post to adjacent posts made up the rigid array. In order to keep all forces calculable, Leighton insisted that all joints be pinned. This resulted in a stiff and homologous structure.

Figure 2. Leighton standing on the back-up structure.

Once the struts and posts were constructed in the shop the support structure was very easy to build. The next problem was how to make the reflecting surface. That was solved by using aluminum honeycomb to produce each of 84 hexagonal panels (the edge panels have a more complex shape) which were fitted together to form the 10.4 meter dish. Each panel was supported from the back-up structure by three adjustable stand-off pins. Each pin was shared by two other adjacent panels. Differential jack screws connected the ends of the pins to the panels. This enabled very fine mechanical control of the surface position.

Figure 3. Details of the back-up structure. Near the center is a support pin and its associated jack-screw.

The upper surface of the honeycomb panels was then shaped by rotating the entire dish on a carefully constructed air bearing, under a cutting tool. This tool ran up and down a precision parabolic track, set by laser interferometry relative to a horizontal level consisting of an oil tray, thus producing the desired parabolic shape. Sheet aluminum of specially made uniform thickness was epoxied to the aluminum honeycomb surface. Finally, the aluminum surface was polished to remove fine-scale variations due to thickness or honeycomb variations. After several iterations of polishing and measurement, the dish achieved a test rms of 10 µm, on the air bearing, in the zenith. A mirror-like finish to the dish may have been desirable, but the dangers of the Sun being imaged on some vulnerable surface precluded this. To minimize this hazard, the surface was polished only until a satin-like finish was achieved. Even so, it has happened that during a testing or construction operation, the Sun was inadvertently focused on a secondary mirror feed leg and melted some electrical cables running along the leg! Thus, great care is needed when exposing the dish to the Sun. This is one of the reasons observations are not routinely made during the daytime, although theoretically possible. Another, and perhaps more immediate, reason is that exposing the dish to the Sun will heat it differentially and cause deterioration of the surface figure. In the case of the 1991 total solar eclipse, Dr. Hal Zirin of Caltech, for his observations, provided a tent-like cover for the dish, transparent to submillilmeter waves but protecting the dish from heating. (See Fig. 44 in the Photo Gallery section)

Figure 4. The feed legs which support the secondary mirror.

Thermal stability is a critical aspect of a metal telescope, and for that reason Leighton used the thermally controlled large building, that had previously housed the Palomar 200 inch mirror, for the CSO dish construction. The dish is constructed so that the surface panels are demountable and the back-up structure is disassembleable into a few easily transportable pieces. Thus, a notable feature is that the dish may be disassembled and reassembled with only a moderate loss of accuracy. The means for adjustment were provided, as mentioned above, by the differential screws at the bottom of each stand-off pin, and also by a warping harness for each panel, and, potentially, by heater coils that had been built into the hexagonal panels. (It is not clear how these heaters were intended to function, and they were never used. Instead, the idea of heating or cooling the stand-off pins connecting the panels to the screw jacks was proposed.) These features were needed because of the plan to build the entire telescope and dome in Pasadena for later disassembly and shipment to Mauna Kea, for reassembly on the mountain. The plan permitted testing, adjustment, and possible modifications to be made near where the industrial and technical services are located. This plan included not only the dish but the entire dome. However, the dish itself was never installed on the alt-azimuth mount until all other construction was completed on Mauna Kea. After shipping and installation on Mauna Kea, the surface accuracy had degraded to 40 µm. The errors were partially removed by spinning the dish in the vertical under a crude replica of the Pasadena parabolic track. The surface measurements were finally made by means of a novel "holography" device designed and built by Serabyn, Phillips, and Masson [3]. Errors detected by these methods were corrected by manually adjusting the differential screws. The telescope was "tuned" to optimize the performace at elevation angles of about 50 degrees. A surface accuracy of about 20 µm was obtained. The concept of heating or cooling the stand-off pins using Peltier units, to make fine adjustments and corrections for sag due to gravity, has been recently successfully implemented by CSO engineer Melanie Leong [4]. The improvement in the efficiency has been about 50% at the highest frequencies.

REFERENCES

[1] Robert B. Leighton "A 10 Meter Telescope for Milllimeter and 
    Submillimeter Astronomy" Technical Report for NSF Grant 
    73-04908, 1978.
[2] David Woody, David Vail, and Walter Schaal "Design, Construction, 
    and Performance of the Leighton 10.4-m-Diameter Radio Telescopes"
    Proceedings of the IEEE, Vol. 82, N0.5, May 1994. 	
[3] E. Serabyn, T.G. Phillips, C.R. Masson "Radio Telescope Surface
    Measurement with a Shearing Interferometer" in URSI Proceedings,
    Holography Testing of Large Radio Telescopes, 1991, 40.	
[4] M. Leong, R. Peng, M. Martin,H. Hirosige,R. Chamberlin, T.G. Phillips 
    "A CSO submillimeter adaptive optics system" in Prodeedings 
    of the SPIE, Volume 6275, 2006, 21L.  	

 

Back ] Up ] Next ]