Mercury-Redstone 1
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Mercury-Redstone 1 (MR-1) was the first Mercury-Redstone uncrewed flight test in
Project Mercury Project Mercury was the first human spaceflight program of the United States, running from 1958 through 1963. An early highlight of the Space Race, its goal was to put a man into Earth orbit and return him safely, ideally before the Soviet Un ...
and the first attempt to launch a Mercury spacecraft with the
Mercury-Redstone Launch Vehicle The Mercury-Redstone Launch Vehicle, designed for NASA's Project Mercury, was the first American crewed space booster. It was used for six sub-orbital Mercury flights from 1960–1961; culminating with the launch of the first, and 11 weeks l ...
. Intended to be an uncrewed
sub-orbital spaceflight A sub-orbital spaceflight is a spaceflight in which the spacecraft reaches outer space, but its trajectory intersects the atmosphere or surface of the gravitating body from which it was launched, so that it will not complete one orbital re ...
, it was launched on November 21, 1960 from
Cape Canaveral Air Force Station Cape Canaveral Space Force Station (CCSFS) is an installation of the United States Space Force's Space Launch Delta 45, located on Cape Canaveral in Brevard County, Florida. Headquartered at the nearby Patrick Space Force Base, the statio ...
,
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. The launch failed in abnormal fashion: immediately after the Mercury-Redstone rocket started to move, it shut itself down and settled back on the pad, after which the capsule jettisoned its escape rocket and deployed its recovery parachutes. The failure has been referred to as the "four-inch flight", for the approximate distance traveled by the launch vehicle.


Test background and launch failure

The purpose of the MR-1 flight was to qualify the Mercury spacecraft and the Mercury-Redstone
launch vehicle A launch vehicle or carrier rocket is a rocket designed to carry a payload ( spacecraft or satellites) from the Earth's surface to outer space. Most launch vehicles operate from a launch pads, supported by a launch control center and ...
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 Mercury-Redstone Project'', p. 8-2.NSSDC Master Catalog page. The flight 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 test used Mercury spacecraft #2 together with Redstone MR-1; its launch location was
Cape Canaveral Air Force Station Cape Canaveral Space Force Station (CCSFS) is an installation of the United States Space Force's Space Launch Delta 45, located on Cape Canaveral in Brevard County, Florida. Headquartered at the nearby Patrick Space Force Base, the statio ...
'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.''The Mercury-Redstone Project'', p. 8-3. On that day, following a normal countdown, the Mercury-Redstone's engine ignited on schedule at 9:00 a.m.
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(14:00 
GMT Greenwich Mean Time (GMT) is the mean solar time at the Royal Observatory in Greenwich, London, counted from midnight. At different times in the past, it has been calculated in different ways, including being calculated from noon; as a cons ...
). However, the engine shut down immediately after lift-off from the launch pad. The rocket only rose about before settling back onto the pad. Alarms were immediately sounded at LC-5, but the Redstone didn't explode. Instead it merely sat in place, after which a strange sequence of events happened."MR-1: The Four-Inch Flight", p. 294. 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 and landed about away. Three seconds after the escape rocket fired, the capsule deployed its
drogue parachute A drogue parachute is a parachute designed for deployment from a rapidly-moving object. It can be used for various purposes, such as to decrease speed, to provide control and stability, or as a pilot parachute to deploy a larger parachute. V ...
; 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. However, the fully fueled and powered-up Redstone was now sitting on LC-5 with nothing securing it to the pad. Various other dangers existed as well, such as the capsule's retrorocket package and the
range safety In the field of rocketry, range safety may be assured by a system which is intended to protect people and assets on both the rocket range and downrange in cases when a launch vehicle might endanger them. For a rocket deemed to be ''off course' ...
destruct charges. 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; this did not occur, however, as the weather conditions were favorable. Amid the panicked atmosphere in the control room, the launch team was unable to come up with quick and viable options to rectify the situation. Flight director
Chris Kraft Christopher Columbus Kraft Jr. (February 28, 1924 – July 22, 2019) was an American aerospace and NASA engineer who was instrumental in establishing the agency's Mission Control Center and shaping its organization and culture. His protégé ...
rejected several unsafe interventions, including using a rifle to shoot holes in the booster's propellant tanks to depressurize them. He eventually took the advice of one of the test engineers to simply wait out the battery discharge and let the oxidizer boil off. This early test failure and subsequent panic led Kraft to declare "That is the first rule of flight control. If you don't know what to do, don't do anything." Technicians therefore waited until the next morning, when the flight batteries in the rocket and capsule had run down and the Redstone's
liquid oxygen Liquid oxygen—abbreviated LOx, LOX or Lox in the aerospace, submarine and gas industries—is the liquid form of molecular oxygen. It was used as the oxidizer in the first liquid-fueled rocket invented in 1926 by Robert H. Goddard, an app ...
had boiled off, before they could work on the rocket and render it safe.


Causes of the failure

Investigation revealed that the Redstone's engine shutdown was caused by two of its electrical cables separating in the wrong order. These cables were a control cable, which provided various control signals, and a power cable, which provided electrical power and grounding. Both cables were plugged into the rocket at the bottom edge of one of its tail fins and would separate at liftoff. The control cable was supposed to separate first, followed by the power cable. However, for this launch, the control cable was longer than expected—it was one designed for the military
PGM-11 Redstone The PGM-11 Redstone was the first large American ballistic missile. A short-range ballistic missile (SRBM), it was in active service with the United States Army in West Germany from June 1958 to June 1964 as part of NATO's Cold War defense of W ...
missile rather than the shorter cable designed for Mercury-Redstone. This control cable had been clamped to compensate for its greater length, but when the vehicle lifted off, the clamping did not work as planned and the control cable separation was delayed, eventually occurring about 29 milliseconds ''after'' the power cable had separated. During this brief interval, the lack of electrical grounding caused a substantial current to flow through an electrical
relay A relay Electromechanical relay schematic showing a control coil, four pairs of normally open and one pair of normally closed contacts An automotive-style miniature relay with the dust cover taken off A relay is an electrically operated switch ...
which was supposed to trigger normal engine cut-off at the end of powered flight. This relay tripped, causing the Redstone to shut off its engine and send a "normal cut-off" signal to the capsule. Under normal circumstances, when the capsule received this signal during a flight, it would do two things: it would jettison its escape rocket, which was no longer of any use, and after the escape rocket had flown clear, fire the explosive bolts holding it to the booster for separation. In the case of MR-1, the capsule did jettison the escape rocket as it was designed to, but the separation sequence did not occur. The capsule was designed to suspend this separation until the vehicle's acceleration had almost ceased, so that the capsule would not be hit by a still-accelerating launch vehicle. This would happen when the capsule's acceleration sensors detected an acceleration approaching 0  g, which it would normally experience after the Redstone had shut down and was entering free fall. However, in MR-1, the Redstone was not in free fall but rather sitting supported on the ground. Thus the capsule sensors detected the effect of their own supported weight, which they read as a constant "acceleration" of 1 g. Because of this apparent acceleration, capsule separation was disabled.''The Mercury-Redstone Project'', p. 8-5. The jettison of the escape rocket activated the capsule's parachute recovery system. Since the altitude was below , this system was triggered by its atmospheric pressure sensors and followed its usual sequence, with the drogue parachute deploying first, followed by the main parachute. But because the main parachute was not supporting the capsule's weight, the parachute system did not detect any load on this chute, so it acted as if the chute had failed and deployed the reserve parachute. Since the Redstone's automatic inflight abort sensing system was running in open-loop mode, the engine shutdown did not trigger an abort. However, the system did report an abort condition, so it did function properly.''The Mercury-Redstone Project'', p. 8-6.


Aftermath

The Redstone had suffered some minor damage from falling back on the pad, but it could still be used after refurbishment, so it was returned to Marshall Space Flight Center in Huntsville,
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, and was held in reserve. A new test flight was scheduled,
Mercury-Redstone 1A Mercury- Redstone 1A (MR-1A) was launched on December 19, 1960 from LC-5 at Cape Canaveral, Florida. The mission objectives of this uncrewed suborbital flight were to qualify the spacecraft for space flight and qualify the system for an upcoming ...
(MR-1A), which would use a new Mercury-Redstone rocket, numbered MR-3. MR-1's Mercury spacecraft, #2, was undamaged, so it was reused for MR-1A, together with the escape rocket from spacecraft #8 and the antenna fairing from spacecraft #10."MR-1: The Four-Inch Flight", p. 296. To prevent a failure like MR-1's from recurring, subsequent Mercury-Redstones added a grounding strap about long to electrically connect the rocket to the launch pad. This strap was designed to separate from the rocket well after all other electrical connections to the ground had been severed. Mercury engineers were also concerned that MR-1's failure had allowed a "normal cutoff" signal to reach the capsule and trigger the premature jettisoning of the escape rocket, since in an actual emergency this would remove the only escape mechanism for the astronaut. Had MR-1 been a crewed mission, the normal contingency would have been a pad abort, lifting the Mercury capsule off the booster and to safety via the escape rocket. Since the escape rocket had instead jettisoned itself from the capsule the astronaut would have been left in a very precarious situation, stuck inside the Mercury capsule atop a fully fueled, fully independently powered, yet completely untethered and partially damaged Redstone booster. To prevent a situation like this, the Mercury-Redstone was altered so that it could not send a "normal cutoff" signal to the capsule until 129.5 seconds after liftoff, about 10 seconds before the expected time of the Redstone's actual engine cutoff. MR-1 was never used for another flight after its return to Huntsville. It was eventually put on display at the Space Orientation Center of Marshall Space Flight Center.


Current location

Mercury spacecraft #2, used in both the Mercury-Redstone 1 and Mercury-Redstone 1A flights, was displayed at the
NASA Ames Exploration Center The NASA Gift Shop in Silicon Valley (also called the NASA Ames Visitor Center) is a visitor center at the entrance of NASA's Ames Research Center in Moffett Field, California. The center has the following exhibits: * The Mercury-Redstone 1A caps ...
,
Moffett Federal Airfield Moffett Federal Airfield , also known as Moffett Field, is a joint civil-military airport located in an unincorporated part of Santa Clara County, California, United States, between northern Mountain View and northern Sunnyvale. On November 10 ...
, near Mountain View,
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. As of July 13th, 2022, it is now on display at the
Cradle of Aviation Museum The Cradle of Aviation Museum is an aerospace museum located in Garden City, New York on Long Island, established to commemorate Long Island's part in the history of aviation. It is located on land once part of Mitchel Air Force Base which, to ...
in Garden City, New York. Other Mercury-Redstone rockets are on display at the U.S. Space & Rocket Center in Huntsville and elsewhere.


Images

File:Mg-KSC-61C-181.jpg, Fueling MR-1 in preparation for launch. File:Mercury-Redstone 1 launch attempt S63-02651.jpg, MR-1 at the moment of ignition. File:Project Mercury-Capsule 2 GPN-2000-000382.jpg, Mercury spacecraft #2 in an unfinished state at Lewis Hangar in 1959. File:Mercury Spacecraft at NASA Ames.JPG, Spacecraft #2, used on both the MR-1 and MR-1A flights, on display at
NASA Ames Exploration Center The NASA Gift Shop in Silicon Valley (also called the NASA Ames Visitor Center) is a visitor center at the entrance of NASA's Ames Research Center in Moffett Field, California. The center has the following exhibits: * The Mercury-Redstone 1A caps ...
File:Mercury MR1-3.jpg, alt=, Mercury-Redstone 1 at Cradle of Aviation Museum.


Notes


References

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Bibliography

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External links

*A series of photos from
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's LIFE magazine photo archive, showing MR-1 jettisoning the escape rocket and deploying the drogue chute


Mercury spacecraft #2 display page on "A Field Guide to American Spacecraft" website.YouTube video of Mercury-Redstone 1 mishap
{{Project Mercury 1960 in spaceflight Project Mercury 1960 in the United States Rocket launches in 1960