Fabrication process for an envelope, in particular for space bal

Details Fabrication process for an envelope, in particular for space bal Fabrication process for an envelope, in particular for space bal

1980-12-22

1983-12-13

Blix, Trygve M.

Aeronautics and astronautics

Aircraft, lighter-than-air

Balloons

244126, B64B 140

Patent

active

044201303

ABSTRACT:
A stress control mechanism for a space balloon is comprised of an axial tie member extending from the upper pole of a load carrying space balloon envelope, the tie member passing from the upper pole of the space balloon envelope through the balloon to an aperture located in a slideable member attached to the lower pole of the space balloon, a stopping member positioned at a pre-selected point on the axial tie member as a member for stopping the slideable member and thereby permitting the space balloon to assume a pre-selected shape upon inflation of the space balloon.

REFERENCES:
patent: 2858090 (1958-10-01), Winzen et al.
patent: 2864569 (1958-12-01), Froehlich
patent: 3182932 (1965-05-01), Winker

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