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: 6/25/1977
Launch site: Grenada, Mississippi, US  
Balloon launched by: National Scientific Balloon Facility (NSBF)
Balloon manufacturer/size/composition: Zero Pressure Balloon Tandem 4.130.000 cuft + 1.250.000 cuft
Flight identification number: 136NT
End of flight (L for landing time, W for last contact, otherwise termination time): 6/25/1977
Balloon flight duration (F: time at float only, otherwise total flight time in d:days / h:hours or m:minutes - ): 1 h
Landing site: Flight aborted at 4000 ft.
Payload weight: 500 lb

This was the third test flight of the system. Sky Anchor III mission was launched from Grenada, Mississippi on June 25, 1977. The launch site was chosen due to the high winds at the float altitude which would not allow sufficient float time from Texas. The balloon system consisted of a 4.130.000 cubic feet zero pressure balloon, a 514 lb payload and a 1.250.000 cubic feet super pressure balloon. Instrumentation included two super 8 mm movie cameras, a load cell, altitude monitors, differential pressure gauge, and a television camera for real time visual monitoring of the system.

The launch of the system went smoothly. However, when the tow balloon, above the super pressure balloon, was cut away at approximately 3,000 feet the ascent stopped. Ballast was then dropped to aid the ascent. The pilot reported a large hole in the wall of the super pressure balloon. The flight was then terminated when the balloon system was over a satisfactory recovery zone. Investigations revealed that when the tow balloon was cut away, the primer cord destruct was activated thus destroying the super pressure balloon.

Investigation in to the failure yielded two possibilities of failure. One was the possibility of a short to the PCM Command Package located between the tow balloon and the top of the super pressure balloon. The other possibility was that of a static discharge. To correct the problem for future flights the command box was moved to the base of the super pressure balloon along with the bottom ballast container.

External references

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