Purpose of the flight and payload description

The Sky Anchor System was a two balloon system developed and tested by the National Scientific Balloon Facility (NSBF), during the 70's and 80's decade as part of a long lasting effort of the agency to develope a long duration balloon system. The concept -originally tested in a small scale in 1963- was boosted by the needs of the scientific ballooning community which could benefit in many areas of interest from longer exposure times at altitude. The final goal of the developmental effort was to built a vehicle capable of transport a 500 lb scientific payload at 130,000 ft for a minimum of 100 days duration.

The Sky Anchor system used a two balloon system on which a conventional zero pressure balloon (open) carried below a super pressure balloon (closed) which acted as ballast and anchor. In the image at left is a basic scheme of the system (a more detailed description can be seen clicking over the drawing).

The theoretical operation of the system was as follows. Once the system was airborne, on the way to the main balloon's operational altitude, the super pressure became filled and pressurized. As the "super pressure" continued to be carried upward it losed more and more lift. When sunset occured the entire system descended to a new equilibrium altitude where the increase in lift on the super pressure balloon just equaled the sunset effect on the main balloon. Although its volume was decreased, no gas was lost from the main balloon. At sunrise, the main balloon expanded and the system once again rose. In so doing the super pressure balloon losed the lift that it gained at sunset and the system stabilized at the same altitude as the preceding day. Since there was no change in suspended weight on the main balloon, it should not overshoot and again there will be no loss of gas. As in the pure super pressure system, assuming there were no leaks, the flight duration was limited only by creep, gas diffusion and ultraviolet degradation of the balloon fabric.

Throughout the development of the program, the actual flight experience turned out to be much more complex than planned, so after mixed results on 14 flights over six years, the program was abandoned in 1982. However, the experience gained would pave the way for other groups to develop more successful designs in the future. This would allow the original goal behind Sky Anchor to be achieved in the early decades of the 21st century.

Details of the balloon flight

Balloon launched on: 1/29/1981
Launch site: Guaratinguetá Air Base, Sao Paulo, Brazil  
Balloon launched by: National Scientific Balloon Facility (NSBF)
Balloon manufacturer/size/composition: Zero Pressure Balloon Raven - 134.561 m3 (12.70 microns) - 56.657 m3 (38.10 Microns bilaminated polyester)
Flight identification number: 174N
End of flight (L for landing time, W for last contact, otherwise termination time): 1/29/1981
Landing site: Main balloon failure
Payload weight: 227 kgs

This was meant to be the twelveth test flight of the system and the first one scheduled to circumnavigate the earth. The balloon system consisted of a 4.750.000 cubic feet zero pressure balloon, a 500 lb payload and a 2.000.000 cubic feet super pressure anchor balloon constructed of 0.75 x 0.75 mil laminated polyester film. Interim long duration power, tracking and data retrieval systems were specially developed for this mission along with two automated ballasting systems. The power system consisted of solar panels in a flat, horizontal array in conjunction with rechargable gel-cell batteries. Primary data retrieval was planned to be through the GOES/Meteosat Satellite System while primary positioning and secondary "housekeeping" data retrieval would be through the ARGOS Satellite System. Secondary positioning would be done through interpretations of data gathered by on-board sensors and transmitted through the GOES system.

Sky Anchor XII was launched from Guaratingueta, Brazil on January 29, 1981, however shortly after launch the zero-pressure balloon failed due to unexpected weather conditions during inflation. Data retrieval at NSBF headquarters in Palestine, Texas through GOES/METEOSAT was excellent during the checkout and short flight.

External references

Images of the mission


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