NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Mercury contamination study for flight system safetyThe effects and prevention of possible mercury pollution from the failure of solar electric propulsion spacecraft using mercury propellant were studied from tankage loading of post launch trajector injection. During preflight operations and initial flight mode there is little danger of mercury pollution if proper safety precautions are taken. Any spillage on the loading, mating, transportation, or launch pad areas is obvious and can be removed by vacuum cleaning soil and chemical fixing. Mercury spilled on Cape Kennedy ground soil will be chemically complexed and retained by the sandstone subsoil. A cover layer of sand or gravel on spilled mercury which has settled to the bottom of a water body adjacent to the system operation will control and eliminate the formation of toxic organic mercurials. Mercury released into the earth's atmosphere through leakage of a fireball will be diffused to low concentration levels. However, gas phase reactions of mercury with ozone could cause a local ozone depletion and result in serious ecological hazards.
Document ID
19730007128
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gorzynski, C. S., Jr.
(Martin Marietta Corp. Baltimore, MD, United States)
Maycock, J. N.
(Martin Marietta Corp. Baltimore, MD, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1972
Subject Category
Space Sciences
Report/Patent Number
RIAS-TR-72-18C
NASA-CR-130286
Report Number: RIAS-TR-72-18C
Report Number: NASA-CR-130286
Accession Number
73N15855
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-953519
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available