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U.S. Department of Energy
Office of Scientific and Technical Information

TRANSMISSION-LINE MISSILE ANTENNAS

Technical Report ·
DOI:https://doi.org/10.2172/4275403· OSTI ID:4275403
Protruding rocket antennas of low silhouette are examined using transmission-line concepts. The theory was developed specifically for nondissipative terminations and line sections; however, the formulas are readily generalized to include ohmic losses in the lines and terminations. Adaptive computations may be made for conductors other than circular and the theory may be used to analyze antennas of other missiles. (J.R.D.)
Research Organization:
Sandia Corp., Albuquerque, N. Mex.
Sponsoring Organization:
USDOE
DOE Contract Number:
AT(29-1)-789
NSA Number:
NSA-13-011790
OSTI ID:
4275403
Report Number(s):
SCTM-436-58(14)
Country of Publication:
United States
Language:
English

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