14th Aerodynamic Decelerator Systems Technology Conference 1997
DOI: 10.2514/6.1997-1514
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The development of a flight termination parachute system for a 1900 lb payload

Abstract: A 30-ft-diameter ringslotholid parachute was designed, developed, and tested at Sandia National Laboratories as the major component of a flight termination system required for a 1900-lb gliding delivery platform. Four full-scale sled tests were performed to validate the design models of the parachute, determine reefing line length, demonstrate structural adequacy of the parachute materials, and demonstrate that performance met the design requirements.

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