Based on the decontamination data given in Chapters 4 and 5, it appears that different WB-29s served as the heavy nuclide sampler on various shots and the shoe boxes were easily moved from one aircraft to another. The B-36H double~squeegee systems had six compressors pumping into six 900-in? (14,743-cm*) containers at 3,000 Lb/in? (211 kg/em?) (Reference 9, An- nex D). The F-84Gs were equipped with a sampling panel mounted atop the main instrument panel. The sampling panel is shown in Figure 24. This panel contained radiac instruments and indicator lights for each sampling system. The rate meter for the tiptank ion chamber Stage scale: (see Figure 24) 0-1 R/hr, 0-10 R/hr, or 0-100 R/hr. had a three- The reading from this meter was transmitted by the pilot to the sampler control aircraft where the sampling project manager maintained control of each mission. The top center of the sampling panel had an integrating dosimeter tegron). (In- The Integron meter recorded the total cockpit dose in the range of 0-7.5 R with an error of +20 percent during sampling missions ence 29, Chapter 8 et seq). (JASPER) IM 71/P0 PATE METER FOR COCKPIT INTENSITY The IM-71/PD (Jasper) INTEGRON = a rate meter measured WINGTIP TANK SAMPLING SYSTEM CONTROL AND INDICATORS aAa Ot a== GAS SAMPLE SYSTEM INOICATORS \ DOS IMETER RATE METER TO WING TANK SNAP SAMPLER CONTROL SWITCH CONTROL STICK Figure 24. F-84G sampling panel, CASTLE. 138 (Refer-