SPEKTROSTRATOSKOP LAUNCH TEST

The SPEKTROSTRATOSKOP was an uncrewed balloon-borne solar observatory developed in late 1960s at the Fraunhofer Institut, in Freiburg im Breisgau, Germany in order to obtain simultaneous pictures and spectra of solar features with the highest possible spectral and spatial resolution. The instrument was manufactured by the firm Carl Zeiss from Oberkochen.

In the image at left we can see an scheme of the instrument (click to enlarge). It combined a telescope with a high-resolution spectrograph and an Ha-Lyot filter. The instrument used a 30.5 cm aperture parabolic mirror with an f/8 ratio and an equivalent focal length of 63 meters. A small Newtonian mirror reflected a 2 x 2 arcminute section of the primary image sideways, which was then magnified twice by a transfer lens system before reaching the spectrograph slit.

The spectrograph was designed in a Littrow configuration and employed a Bausch & Lomb diffraction grating with a 16 x 21 cm ruled surface and 600 lines per millimeter. It operated in the fourth order for Ha and fifth order for green light, achieving a spectral resolution of approximately 400,000. The system included two transfer lens systems that reimaged both the primary spectrum and the light reflected from the slit jaws onto separate camera film planes with 12.5x magnification.

The instrument incorporated a Lyot filter that could be inserted into the f/200 beam near one of the transfer lens systems. A dichroic beam splitter placed before the Lyot filter provided an additional white light image that was used for both television transmission to the ground and the fine guidance system.

The final images measured 24 x 36 mm, while the spectra were 24 x 72 mm. The system achieved a dispersion of about 10 mm per angstrom and an angular scale of 3.3 arcseconds per mm. This translated to spatial and spectral resolution limits of 0.3-0.4 arcseconds and 12 mA for every 0.1 mm on the film.

The instrument package was supported at its center of gravity by a spherical oil-pressure bearing and featured three torque motors for pitch, yaw, and roll control. A second oil-pressure bearing at the top of the supporting frame helped decouple the instrument from balloon movements. The system employed a three-stage guidance system: a coarse guidance that oriented the frame toward the sun, an intermediate guidance using a limb sensor for pointing accuracy within 1 arcsecond, and a fine guidance system using granulation tracking that achieved 0.1 arcsecond precision.

To address focus variations caused by temperature changes, the instrument included an automatic focusing system that used a pinhole scanner to monitor granulation contrast. The total weight of the instrument was kept under one ton

Balloon launched on: 10/6/1966 at 8:20 CST
Launch site: Columbia Scientific Balloon Facility, Palestine, Texas, US  
Balloon launched by: NCAR National Scientific Balloon Flight Station
Balloon manufacturer/size/composition: Zero Pressure Balloon Winzen - Tandem system with Viron 2.94, sleeved - 110.000 cuft (2.0 mil.Stratofilm)
Flight identification number: 255PT
End of flight (L for landing time, W for last contact, otherwise termination time): 10/6/1966
Landing site: No flight. Launch rehearsal
Payload weight: 4418 lbs.
Overall weight: 5695 lbs.

As part of the support by NCAR to the Spektrostratoskope project, a launch system was developed which enabled the NCAR facility to launch the instrument on a tandem balloon system with accelerations well below 1 g. The system permited the balloon train to be reoriented after inflation in the event of a shift of wind. Thus, the objective of the flight was to conduct inflation and launch test of the proposed Spektrostratoskop method and to prepare system for launch, release the balloon and destruct the balloon shortly after.

• Balloon Flight Record Facilities for Atmospheric Research Nº 2, Winter 1966/67
• NCAR Scientific Balloon Facility Annual Report, 1966 National Center for Atmospheric Research, January 1967