sisplest to accomplish. The system is intemted ta accept data frm— seutrca, gamma-ray, thermal, and X-ray transducers ani transform such data to a fora suitable for transmission ani recording. It also is to provide aonitoring of warhead command fimctions and the high-resolution telemetry systea. With the exception of radiation effects, couditions surrounding the Bardtack tests were not greatly different from standard light-missile tesis. accelerations experienced did not exceed 65 g‘s, and space was sufficient to utilize standard components. The effects of radiation were not well under- stood, but cests during Operation Plumbbob indicated that no great difficulties sbould be anticipated at the ranges from burst which were planned for the Program 32 instrument carriers. 9.4.2 Description of System The system will not be described in great detail, since the techniques are well known and couponents are commercially available. Figure 9.€ is a block diagram of a typical instmomentation rocket installation. The principal components in the system are as follows: (1) Bendix TOE-31 subcarrier oscillators (2) Bendix TXv-13 transmitter (3) Rheem REL-09 power amplifier (4) Carter Magnotor 250 v-250 na (5) Ni-Cad ZHIO batteries (6) Sandia-designed, nose-probe antenna (7) ASCOP cocoutation switch accuracy of the system was expected to be better than 5 percent from data input to reduced data. _ The receiving station was mounted in a 34-foot trailer van and consisted of standard cocemercial equipment. receiving station. Figure 9.9 is a block diagras of the FM-™M Its principal items are: (1) ASCOP preamplifiers (2) ASCOP sulticouplers (3) Nems-Clarke Model 1400, erystal-coatrolled receivers (4) Aapex F2 114 cape recorders k)' (5) Miller Model J, 30-channel oscillogragh