Mercury-Redstone 1 - Mission Background and Launch Failure

Mission Background and Launch Failure

The purpose of the MR-1 mission was to qualify the Mercury spacecraft and the Mercury-Redstone launch vehicle for the sub-orbital Mercury mission. It would also qualify the spacecraft's automated flight control and recovery systems, as well as the launch, tracking, and recovery operations on the ground. The mission would also test the Mercury-Redstone's automatic inflight abort sensing system, which would be operating in "open-loop" mode. This meant that the abort sensing system could report a condition requiring an abort, but it would be unable to actually trigger an abort itself. Since the flight did not have a living passenger, this would not pose a safety problem, and it would prevent a faulty abort signal from prematurely ending the flight.

The mission used Mercury spacecraft #2 together with Redstone MR-1; its launch location was Cape Canaveral Air Force Station's Launch Complex 5. An early launch attempt on November 7 was canceled due to last-minute problems with the capsule, so launching was rescheduled for November 21.

On that day, following a normal countdown, the Mercury-Redstone's engine ignited on schedule at 9:00 a.m. Eastern Standard Time (14:00 GMT). However, the engine shut down immediately after lift-off from the launch pad. The rocket only rose about 4 inches (10 cm) before settling back onto the pad. It wobbled slightly, but stayed upright and did not explode. An odd series of events then took place.

Immediately after the Redstone's engine shut down, the Mercury capsule's escape rocket jettisoned itself, leaving the capsule attached to the Redstone booster. The escape rocket rose to an altitude of 4,000 feet (1,200 m) and landed about 400 yards (370 m) away. Three seconds after the escape rocket fired, the capsule deployed its drogue parachute; it then deployed the main and reserve parachutes, ejecting the radio antenna fairing in the process.

In the end, all that had been launched was the escape rocket. Meanwhile, a fully fueled, slightly wrinkled Redstone and its Mercury capsule sat on the launch pad, both with full batteries and live pyrotechnics. Among these pyrotechnics were the capsule's retrorockets and the Redstone's self-destruct system, which was still active. Furthermore, the capsule's main and reserve parachutes were hanging down the side of the rocket, threatening to tip it over if they caught enough wind. Fortunately, the weather conditions were favorable. Technicians had to wait until the next morning, when the flight batteries in the rocket and capsule had run down and the Redstone's liquid oxygen had boiled off, before they could work on the rocket and render it safe.

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