Astronomical balloon-borne telescopes have the potential to improve seeing over ground-based telescopes, but are
compromised by their instability. A one-meter telescope in the Earth's stratosphere could achieve diffraction-limited
seeing superior to the performance of any ground-based telescope in optical or UV wavelengths. If the stability issues
could be addressed, such a telescope could be used for a variety of scientific purposes, including high- resolution optical
imaging, or infrared imaging of targets that are usually precluded from ground-based systems, such as Jupiter, Saturn or
Venus. An image stabilization system was developed with the goal of maintaining the position of the image to within 0.1
arcseconds on the focal plane during image acquisition. This effort requires both deriving an error signal and applying
that error signal to a corrective element. Using a control loop with an optical reference provides a greater bandwidth than
an inertial reference and improves control of high frequency vibrations. The control feedback signal was generated by
monitoring the position of an image using a lateral effect cell. A fine steering mirror was used as a diagonal flat to
control the position of the image and correct for small disturbances in pointing. To evaluate the system, vibration was
induced in a synthetic image and the resultant motion of the image measured. The system was implemented and tested
on a 14-inch f/10 Schmidt-Cassegrain telescope. Large disturbances were attenuated by a factor of 10-100, with a noise
level of less than 2 arcseconds on the test telescope.
A terrestrial stratospheric telescope is ideally suited for making infrared observations of Venus' night hemisphere during
inferior conjunctions. The near-space environment at 35 km altitude has low daytime sky backgrounds and lack of
atmospheric turbulence, both of which are necessary for observing Venus' night side at the diffraction limit when Venus
is close to the Sun. In addition, the duration of the observing campaign will be around 3 weeks, a time period that is
achievable by current long duration flights. The most important advantage, however, will be the ability of a balloonborne
telescope to clearly image Venus' night side continuously throughout a 12-hr period (more for certain launch site
latitudes), a capability that cannot be matched from the ground or from the Venus Express spacecraft currently in orbit
around Venus. Future missions, such as the Japanese Venus Climate Orbiter will also not be able to achieve this level of
synoptic coverage. This capability will provide a detailed, continuous look at evolving cloud distributions in Venus'
middle and lower cloud decks through atmospheric windows at 1.74 and 2.3 μm, which in turn will provide
observational constraints on models of Venus' circulation.
The science requirements propagate to several aspects of the telescope: a 1.4-m aperture to provide a diffraction limit of
0.3" at 1.74 μm (to improve upon non-AO ground-based resolution by a factor of 2); a plate scale of 0.1" per pixel,
which in turn requires an f/15 telescope for 13 μm pixels; pointing and stability at the 0.05" level; stray light baffling; a
field of view of 2 arc minutes; ability to acquire images at 1.26, 1.74 and 2.3 μm; and ability to operate aloft for three
weeks at a time. The specific implementations of these requirements are outlined in this paper. Briefly, a 1.4-m
Gregorian telescope is proposed, with stray light baffling at the intermediate focus. A three-stage pointing system is
described, consisting of a coarse azimuthal rotator, a moderate pointing system based on a star tracker and ALT/AZ
gimbals, and a fine pointing system based on analog photodiodes and a fine steering mirror. The science detectors are
not discussed here, except to specify the requirement for moderate resolution (R > 1000) spectroscopy.
KEYWORDS: Telescopes, Space telescopes, Optical instrument design, Motion models, Control systems design, 3D modeling, Device simulation, Adaptive optics, Domes, Control systems
Studies by Mark Swain and a colleague at the Max Planck Institut fur Astronomie, coupled with results from past and ongoing projects at Harvey Mudd College, strongly suggest that it may be possible to achieve imaging performance comparable to the Hubble Space Telescope at relatively low cost using available, commercial products. This is achievable by placing a 2.4 m telescope, with readily available adaptive optics, on a 30 m tower located at a high-elevation geological "dome" in Antarctica. An initial project surveyed relevant tower design approaches, then generated and evaluated six concept designs for telescope towers. Using data for typical and extreme wind at Dome C to generate wind loads, finite element analysis yielded lateral deflections at the top of 0.3 mm for typical winds and 12.1 mm for extreme gusts, with the lowest resonant frequency at 0.7 Hz; some tower concepts are innovative and allow for easy shipment, setup, and relocation. A subsequent project analyzed a tower designed by Hammerschlag and found fundamental resonance frequencies at 4.3 Hz for bending and 5.9 Hz for torsion; this project also designed and simulated an active telescope control system that maintained 17 milliarcsecond pointing error for the telescope atop the tower during typical wind conditions.
In realizing the scientific potential of locating an astronomical interferometer at one of the Antarctic domes, it will be necessary to retire risks and reduce costs. One way of doing this is to build the interferometer away from Antarctica, test the instrument, and then transport the system as modules to the final location. This novel approach can only be undertaken after it has been shown that such a system will survive the trip without damage, and that calibration of the system will be possible at a very low cost. The authors undertook such a study, measuring the shocks likely to be encountered during shipment, and then establishing that in all but one case, the shocks can be reduced by commercially available vibration isolators to <5g. The one shock not reducible to <5g occurred when the instrument was transferred from an icebreaker to the ice, and will require more careful handling by the shippers. The team also developed and modeled configurations for the delay lines and optics tables to reduce shipment risk while providing a backbone for the delay lines. The study supports the feasibility of a "preassembled" Antarctic interferometer.
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