Serious guidance problem is introduction of amplitude-modulated (AM) or phase-modulated (PM) noise onto transmitted signal by rocket exhaust plume; results of set of measurements wherein X-band attenuation was measured simultaneously with AM/PM noise for seven different double-base propellant systems and single rubber-base system; results are reported for total attenuation and AM/PM noise, together with spectral distributions of noise, generally between 3.9 and 40 kc.
Rocket exhaust plume radar attenuation and amplitude/phase noise
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 4 , n 6 ; p 774-780
1967
7 pages
Article (Journal)
English
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