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—-----------------------------------------------------------------------------------  space division CHRYSLER ---------
                                                                                          iMy CORPORATION



                   Position SENIOR PRODUCT ENGINEER (LG 20)

                   Name        R, J, Theodor off_______________________  Clearance          SECRET______________

                   Degree(s) B ,S. A.E ,                                 Professional Experience Years


                   Education

                        B.S., Aeronautical Engineering, Purdue University, 1958


                   Experience

                        Mr. Theodoroff is a lead engineer in the Structural Design Section, Structures &
                    Mechanics Engineering Department. During the past three years, he has been actively
                    engaged in structural and mechanical preliminary design studies on a recoverable data
                    capsule, an earth orbital stage resupply study, a LEM experiment integration study for
                    an Apollo mission program, and the Voyager Spacecraft. His most recent applicable
                    assignment was to perform the structural stiffness and stress analysis of a film storage
                    and transport mechanism housing.

                        He has extensive experience in the design of missile and airframe structures, having
                    designed the upper nose cone for the Saturn IB-203 vehicle and supervised the production
                    of drawings required to document the final release configuration. For thirteen months, he
                   was responsible for the supervision of a structural design group consisting of five engineers
                    and two layout draftsmen. He designed the shroud outrigger doors, the purge line and
                    electrical quick-disconnect brackets, and the water quench system support structure for
                    the Saturn I, Block I vehicles. He also designed the upper and lower segmented rings, the
                    fin support fittings, and the joints where these were joined by the outriggers, shrouds, and
                    fins for the Saturn I, Block II vehicles. In addition, he completed an extensive redesign of
                    the second stage adapter for Block II and for more than a year he monitored all structural
                    design changes to the S-IV stage for the MSFC Structural Design Branch.

                         Previous to November 1959, he was employed by North American Aviation Company,
                   where he designed stainless steel honeycomb air inlet duct panels, fusel age skin panels,
                    and canted bulkhead ring caps for the F-108 fighter; and by Douglas Aircraft Company,
                    where he assisted in the design of floor and skin panels, frames, and bulkheads for the DC-
                    8 jet airliner.


















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