RR Auction: Space & Aviation Auction

Apollo Inertial Measurement Unit Inertial Rate Integrating Gyro mockup (inoperative shell only), measuring approximately 5.25? tall by 2.5? in diamete

LM Descent Engine shut-off valve assembly for the fuel side, measuring approximately 6 x 6.5 x 7.75. Engraved on the top, “MIR 43625,” with parts numb

Display model of the Lunar Excursion Module Descent Engine (LEMDE) three-motor throttle actuator, circa 1966, measuring 13.5 x 7 x 5, with an affixed

Marquardt R-4D RCS rocket engine combustion chamber, 3.75 x 6, labeled on the side in white stenciling, “S28TC3214.” Side of upper rim engraved, “VN,

Kennedy Space Center Saturn S-IVB Upper Stage Measuring and RF Indicator Panel, measuring approximately 19 x 17.5 x 18, labeled at the bottom of the f

Tank manufactured by Bell Aerosystems Company, measuring approximately 12 x 28 x 14, with a parts label reading: “Item Name: Thank MMH Positive Expuls

Saturn V First Stage LOX Tanking Computer Interface that connected to the Propellant Tanking Computer System, 19 x 14 x 22, labeled at the bottom of t

Apollo post-landing vent valve component, measuring approximately 8.5 x 12 x 7, consisting of a valve gate, actuator rotary, and mounting bracket. The

Saturn V launch vehicle Exploding Bridge Wire (EBW) Firing Unit mounted on a 20 x 8 plywood board, with a George C. Marshall Space Flight Center metal

Apollo A7L Spacesuit Communications Cable Adapter (CCA) breakout box, measuring approximately 17 x 4 x 3 with two 18? long cables extending from one s