Parachute suspended solar pointing control systemA high altitude parachute suspended solar pointing control system has been developed and flight tested for use in the altitude range of 30 to 70 kilometers. This development provides an opportunity for extended solar observations at altitudes higher than that attainable by helium balloons. The new system utilizes the NASA high altitude cross parachute to slow the descent of a rocket launched payload allowing observations in the region of interest. Solar pointing is established by using solar sensors in conjunction with a servo controlled platform and cold gas thrusters for payload roll control. The inherent spin of the cross parachute is decoupled by a swivel joint attached to the parachute suspension lines. This paper describes the design, test and flight performance of the new system.
Document ID
19820064508
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Sakoda, G. T. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Fujimoto, R. J. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Shigemoto, J. M. (Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Windsor, R. M. (NASA Goddard Space Flight Center Greenbelt, MD; Lockheed Missiles and Space Co., Inc., Sunnyvale, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 82-1733Report Number: AIAA PAPER 82-1733