Publication Date:
2019-06-28
Description:
A balloon-borne winch system has been developed and flight tested which permits the repetitive lowering and hoisting of a stratospheric sampling payload for distances of up to 20 km from a float altitude of 35-40 km. This new approach to in situ stratospheric measurements permits multiple scans of various depths and velocities, closely spaced over a period of hours or days, thus dramatically increasing observational effectiveness. The motor driven winch permits control of ascent velocities from 0-9 m/s with energy derived from a large battery; for descent, the motors are used as generators, velocity is controlled over the same range, and the energy is dumped radiatively to space. The 1.75 mm diameter tether is of braided Kevlar construction with a nylon jacket; it exhibits a 2900 N break strength. Both the winch and the payload suspended by the tether are fully instrumented to evaluate potentially destructive system-induced dynamics and the effects of stratospheric wind shears. The system was successfully flight tested by lowering a 62 kg payload for a distance of 12 km from a float altitude of 38.5 km and hoisting it back up again, both at velocities ranging between 5-9 m/s. Observations indicated minimal system-induced dynamical effects, and no adverse effects due to the 8 m/s wind shear present during flight.
Keywords:
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Type:
AIAA PAPER 84-0027
Format:
text
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