of transistor and the retrorocket heat shields were redesigned. The MIDAS program was temporarily suspended at this point when a committee headed by ARPA director Jack Ruina recommended that no attempt at an operational missile early warning system be made until the Air Force demonstrated that it was a feasible concept at all; in addition, Midas's sensors were designed to detect liquid-fueled rocket exhaust, not solid-fueled exhaust, which was now widely seen as the future of ballistic missiles (as things would have it, the Soviet Union was far behind the United States in development of solid-fueled rockets). The committee found that program management of MIDAS was "awful" and at the current rate of success, "it would take ten years to develop an operational system". In November 1961, the Defense Department issued a directive placing all DoD space programs under strict secrecy, and so MIDAS was given the cover name "Program 461". The development time of the program was also lengthened to give more space to work out problems with the hardware. Despite these changes, the failures kept coming. After a six-month gap, MIDAS 5 orbited on April 9, 1962. The Atlas autopilot generated an insufficient pitch and roll program, resulting in excessive altitude and insufficient velocity. This prevented the normal guidance system cutoff commands from being sent so SECO was caused by propellant depletion while a backup command from the programmer performed VECO and Agena separation. MIDAS 5 reached orbit, but an improper one from what was planned. The satellite operated until orbit 7 when a battery failure resulted in insufficient power for continued operation of the satellite systems. An extensive investigation into the Atlas autopilot malfunction found that the gyroscopes had transmitted low signal gain in all three axes, but failed to determine a specific cause. Several changes to preflight procedures and improved testing of gyroscope packages resulted. Eight months later, MIDAS 6 lifted off (December 17) but never made it to orbit. The flight was apparently normal until loss of flight control starting at T+77 seconds. The Atlas broke up at T+80 seconds, the Agena continuing to transmit signals until impact in the ocean approximately 4.7 minutes after launch. Investigation into the cause of the malfunction was hampered by limited flight data--the Atlas's telemetry transmitter antenna had failed during the prelaunch countdown. Tracking film revealed a puff of smoke at the Atlas's tail end at T+64 seconds, and