Mercury-Redstone 3

Information about Mercury-Redstone 3

Mercury-Redstone 3
Mission insignia
Freedom 7 insignia
Mission statistics
Mission name:Mercury MR-3
Call sign:Freedom 7
Number of
crew members:
1
Launch:May 5, 1961
14:34:13 UTC
Cape Canaveral
Complex 5
Landing:May 5, 1961
14:49:41 UTC
27.23° N 75.88° W
Duration:15 min 22 s
Number of
orbits:
Suborbital
Apogee:116.46 mi
187.42 km
Distance
traveled:
302.77 mi
487.26 km
Maximum
velocity:
5,143 mph
8 277 km/h
Peak acceleration:11 g (108 m/s²)
Mass:
Launch
Apogee
Reentry
Landing

1 832.64 kg
1 295.07 kg
1 169.81 kg
1 050.53 kg
Crew picture
Enlarge picture
Mercury 3 crew portrait (Shepard)
Alan Shepard


Mercury-Redstone 3 was a U.S. Mercury program manned space mission launched on May 5, 1961 using a Redstone rocket, from Launch Complex 5 (LC-5) at Cape Canaveral, Florida. The Mercury capsule was named Freedom 7 and it performed a suborbital flight, piloted by astronaut Alan Shepard—the first American in space. The flight lasted less than 16 minutes and attained an altitude of just over 187 km.

Unlike the earlier Soviet Vostok 1 flight, Shepard did not orbit the earth but simply went up and down which requires a less powerful rocket and simpler guidance. He did however became the first astronaut to return to Earth with his ship, while the Russian cosmonaut parachuted away from his during landing. Soviet Premier Nikita Khruschev criticized Freedom 7 as a mere 'flea hop' compared to the recent flight of Vostok 1 and its passenger Yuri Gagarin.

Crew

  • Alan Shepard (1)
*Number in parentheses indicates number of spaceflights by each individual prior to and including this mission.

Backup crew

Mission parameters

  • Mass: 1,295 kg (apogee)
  • Maximum Altitude: 187.42 km
  • Range: 487.26 km
  • Launch Vehicle: Redstone rocket

Mission highlights

The Freedom 7 spacecraft had been delivered to Cape Canaveral on December 9, 1960. Freedom 7 was capsule # 7, and it had been given special attention at the factory since it was selected for the first manned suborbital flight in October, 1960. It had originally been expected to be ready for launch almost immediately. However, 21 weeks of unplanned preparation would be needed before it could be launched on its mission. Reaction control system rework was responsible for postponement of the launch until at least March 6, 1961. Damaged and corroded peroxide lines that needed replacement forced a further delay of eight days. The simulated mission test needed to be rerun and structural and equipment defects corrected. The MR-3 mission was finally ready to be launched on May 2, 1961.

Three astronauts had been chosen as finalists to fly the MR-3 mission in January, 1961, and on February 22, 1961 their names were announced to the public. The three were Alan Shepard, Gus Grissom and John Glenn. The public was not told who would actually fly the mission until after a May 2, 1961 launch attempt was cancelled due to weather. It was then revealed that Shepard had been suited up and waiting for 3 hours in Hangar "S" at Cape Canaveral for the launch. The May 2 launch was cancelled 2 hours and 20 minutes before launch, due to weather conditions.

In the early morning of May 5, 1961, Alan Shepard donned his pressure suit with the assistance of technician Joe W. Schmitt. A transfer van carried him to the launch pad, and he ascended the gantry at 10:15 UTC. At 10:21 UTC he entered Freedom 7, and the gantry crew helped attach the harness and hose connections. He would spend the next four hours in the capsule waiting for the launch.

At 9:34 AM EST (14:34 UTC), there were 45 million Americans watching and listening live to their televisions, when at about two seconds after liftoff Alan Shepard reported, "Ahh, Roger; lift-off and the clock is started . . Yes, sir, reading you loud and clear. This is Freedom 7. The fuel is go; 1.2 g [12 m/s²]; cabin at 14 psi [97 kPa]; oxygen is go . . Freedom 7 is still go!" He was riding on Redstone MRLV-7 and in Mercury spacecraft # 7. In all subsequent Mercury flights, the number 7 was appended to the astronaut-chosen spacecraft/mission name and call sign, in honor of the fact that there were 7 original Mercury astronauts.

At T+16 seconds (where T is the time of launch) the Pitch Program started and the Redstone began a 2 deg/s pitch over, from 90 to 45 degrees. At about T+40 seconds, the Pitch Program was complete. Max-Q was reached at 1 minute 24 seconds into the flight when Freedom 7 experienced a maximum dynamic pressure of 580 lbf/ft² (2.8 kPa). During ascent the cabin pressure sealed off at 5.5 lbf/in² (38 kPa) of pure oxygen. At 2 minutes into the flight, Shepard experienced 6 g (59 m/s²) of acceleration.
Enlarge picture
Launch of the Mercury-Redstone 3 spacecraft on May 5, 1961, 9:34 a.m. EST, with Alan Shepard onboard.
The Redstone's engine shut down on schedule at 2 minutes 21.8 seconds. Outside the spacecraft, its shingle temperature reached 220 °F (104 °C). Inside, the cabin was 91 °F (33 °C) The temperature inside Shepard's pressure suit was 75 °F (24 °C). Escape Tower separation, occurred 2 minutes and 22.2 seconds after launch. This is 1 second earlier than nominal, and there was some indication from the recovered escape tower that the jettison rockets had been fired manually. Shepard said he did not remember pulling the manual "JETT TOWER" override ring.

Three Posigrade Rockets with 370 lbf (1.6 kN) thrust each, fired for 1 second and separated the spacecraft from the Redstone booster at a rate of 15 ft/s (4.6 m/s) at 2 minutes 32.3 seconds after launch. At 3 minutes the automatic attitude control system (AACS) rotated the spacecraft 180 degrees, to a heatshield-forward position. The spacecraft remained in this position for the remainder of the flight. The spacecraft had almost reached apogee in its ballistic flight.

Shepard took manual control of the spacecraft attitude, one axis at a time, from the automatic attitude control system. The first thing he did was position the spacecraft to its retrofire attitude of 34 degrees pitch (nose of spacecraft pitched down 34 degrees). He then tested manual control of yaw and roll. When he took control of all three axes, he found that the spacecraft response was about the same as that of the Mercury simulator.

He then made observations outside the spacecraft, using the two porthole windows and the periscope. He saw the outlines of the west coast of Florida and the Gulf of Mexico. Lake Okeechobee, in central Florida, was also visible, but he could not see any city. Andros Island and the Bahamas were also observed in the periscope.

The retrorockets were fired at about T+5 minutes and 15 seconds into the flight, shortly after the spacecraft reached an apogee of 116.5 miles (187 km). The three 1000 lbf (4.4 kN) thrust retrograde rockets ripple-fired to provide a 510 ft/s (155 m/s) delta-V in the opposite direction of travel. Each retrorocket fires for a total of 10 seconds. They are fired 5 seconds apart so they overlap in burning (Retro #1 fired at 5:14.1; Retro #2 fired at 5:18.8 and Retro #3 fired at 5:23.6 MET). The retrorocket firing could be easily heard, but the noise was not as loud as the sound of the jet trainers he had flown. The periscope was retracted at T+5 minutes and 45 seconds and the retropack was jettisoned at about T+6 minutes and 13.6 seconds. After retrofire the nose of the spacecraft was pitched up to a 14 degree from Earth-vertical attitude for reentry. This happened at about T+6 minutes and 20 seconds.

During the descent, Shepard tried to look out the awkwardly placed porthole windows to observe the stars. He could see nothing, not even the horizon. At about T+7 minutes and 48.2 seconds, the 0.05 g (0.5 m/s²) light came on, an indication that the acceleration buildup was about to start. The Automatic Stabilization & Control System (ASCS) detected the beginning of reentry and initiated a 10 deg/s roll. This maneuver makes the spacecraft more stable during reentry. During reentry a peak of 11.6 g (114 m/s²) was reached.

At 21,000 ft (6.4 km) about T+9 minutes and 38.1 seconds after launch, the drogue parachute came out, at 15,000 ft (4.6 km) a snorkel valve opened to equalize cabin pressure with the outside air. At 10,000 ft (3 km), about T+10 minutes and 14.8 seconds into the flight, the antenna canister at the top of the spacecraft jettisoned as planned, pulling out the main parachute. About 5 seconds later, the beryllium heatshield dropped down four feet (1.2 m), extending the landing bag under the spacecraft. Freedom 7 was descending under the parachute at 35 ft/s (11 m/s).

Splashdown occurred at T+15 minutes and 22.0 seconds. Water impact was comparable to landing a jet aircraft on an aircraft carrier. Freedom 7 tilted over on the right side, about 60 degrees from an upright position. Shepard checked the spacecraft interior for leaks, but found none. Slowly, Freedom 7 came to an upright position, taking about a minute to do so.

Enlarge picture
Mercury 7 patch created subsequent to the mission.
A recovery helicopter that had been watching Freedom 7 for five minutes of its descent now came overhead and hooked a cable to the top of the spacecraft. The helicopter crew was in radio communications with Shepard. The astronaut indicated he would release the spacecraft hatch when it had cleared the water. The helicopter pulled the spacecraft a couple of feet (about 1 m) higher in the water and Shepard released the hatch. A sling was lowered to the astronaut and he was lifted into the helicopter. Both Shepard and the Freedom 7 were then flown to the deck of the nearby recovery carrier, the USS Lake Champlain. They were onboard the carrier 11 minutes after landing in the water. The astronaut and spacecraft came through the flight in fine shape.

The flight lasted 15 minutes 28 seconds, and the spacecraft traveled 302 miles (486 km) from its launch point, ascending to 116.5 miles (187 km). Freedom 7 landed at these coordinates: . It reached a speed of 5,180 mph (8,754 km/h). During the launch phase, Shepard experienced 6.3 g (62 m/s²) and during reentry 11.6 g (114 m/s²).

Following the flight the capsule was examined by engineers and found to be in excellent shape; so much so that they decided it could have been safely used again in another launch. The Freedom 7 is now on display in the lobby of the Armel-Leftwich Visitor Center, at the U.S. Naval Academy, Annapolis, MD. It was placed there after Shepard's death in 1998.

Flight events

T+ TimeEventDescription
T+00:00:00LiftoffMercury-Redstone lifts off, onboard clock starts.
T+00:00:16Pitch ProgramRedstone pitches over 2 deg/s from 90 deg to 45 deg.
T+00:00:40End Pitch ProgramRedstone reaches 45 deg pitch.
T+00:01:24Max QMaximum dynamic pressure ~575 lbf/ft² (28 kPa).
T+00:02:20BECORedstone engine shutdown - Booster Engine Cutoff. Velocity 5,200 mph (2.3 km/s)
T+00:02:22Tower JettisonEscape Tower Jettison, no longer needed.
T+00:02:24Capsule SeparationPosigrade rockets fire for 1 s giving 15 ft/s (4.6 m/s) separation.
T+00:02:35Turnaround ManeuverCapsule (ASCS) system rotates capsule 180 degrees, to heat shield forward attitude. Nose is pitched down 34 degrees to retro fire position.
T+00:05:00ApogeeApogee of about 115 miles (185 km) reached at 150 miles (240 km) downrange from launch site.
T+00:05:15RetrofireThree retro rockets fire for 10 seconds each. They are started at 5 second intervals, firing overlaps. Delta v of 550 ft/s (168 m/s) is taken off forward velocity.
T+00:05:45Retract PeriscopePeriscope is automatically retracted in preparation for reentry.
T+00:06:15Retro Pack JettisonOne minute after retrofire retro pack is jettisoned, leaving heat shield clear.
T+00:06:20Retro Attitude Maneuver(ASCS) orients capsule in 34 degrees nose down pitch, 0 degrees roll, 0 degrees yaw.
T+00:07:150.05 g (0.5 m/s²) Maneuver(ASCS) detects beginning of reentry and rolls capsule at 10 deg/s to stabilize capsule during reentry.
T+00:09:38Drogue Parachute DeployDrogue parachute deployed at 22,000 ft (6.7 km) slowing descent to 365 ft/s (111 m/s) and stabilizing capsule.
T+00:09:45Snorkel DeployFresh air snorkel deploys at 20,000 ft (6 km). (ECS) switches to emergency oxygen rate to cool cabin.
T+00:10:15Main Parachute DeployMain parachute deploys at 10,000 ft (3 km). Descent rate slows to 30 ft/s (9 m/s)
T+00:10:20Landing Bag DeployLanding bag deploys, dropping heat shield down 4 ft (1.2 m).
T+00:10:20Fuel DumpRemaining hydrogen peroxide fuel automatically dumped.
T+00:15:30SplashdownCapsule lands in water about 300 mi (500 km) downrange from launch site.
T+00:15:30Rescue Aids DeployRescue aid package deployed. The package includes green dye marker, recovery radio beacon and whip antenna.

References

May 5 is the 1st day of the year (2nd in leap years) in the Gregorian calendar. There are 0 days remaining.

Events

  • 553 - The Second Council of Constantinople begins.

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19th century - 20th century - 21st century
1930s  1940s  1950s  - 1960s -  1970s  1980s  1990s
1958 1959 1960 - 1961 - 1962 1963 1964

Year 1961 (MCMLXI
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Coordinated Universal Time (UTC) is a high-precision atomic time standard. UTC has uniform seconds defined by International Atomic Time (TAI), with leap seconds announced at irregular intervals to compensate for the earth's slowing rotation and other discrepancies.
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Cape Canaveral from the spanish Cabo Cañaveral, is a headland in Brevard County, Florida, United States, near the center of that state's Atlantic coast at and is also 45 minutes East of Orlando by car.
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Cape Canaveral Air Force Station Launch Complex 5 (LC-5) was a Launch Site at Merritt Island, Cape Canaveral, Florida. The site was used for various Redstone and Jupiter launches.
..... Click the link for more information.
May 5 is the 1st day of the year (2nd in leap years) in the Gregorian calendar. There are 0 days remaining.

Events

  • 553 - The Second Council of Constantinople begins.

..... Click the link for more information.
19th century - 20th century - 21st century
1930s  1940s  1950s  - 1960s -  1970s  1980s  1990s
1958 1959 1960 - 1961 - 1962 1963 1964

Year 1961 (MCMLXI
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A sub-orbital spaceflight (or sub-orbital flight) is a spaceflight in which the spacecraft reaches space, but its trajectory then intersects the atmosphere or surface of the gravitational body from which it was launched, and thus does not enter a stable orbit.
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Motto
"In God We Trust"   (since 1956)
"E Pluribus Unum"   ("From Many, One"; Latin, traditional)
Anthem
..... Click the link for more information.
Project Mercury was the first human spaceflight program of the United States. It ran from 1959 through 1963 with the goal of putting a man in orbit around the Earth. The Mercury-Atlas 6 flight on February 20, 1962 was the first Mercury flight to achieve this goal.
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human spaceflight is a spaceflight with a human crew, and possibly passengers. This makes it unlike robotic space probes or remotely-controlled satellites. Human spaceflight is sometimes called manned spaceflight
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May 5 is the 1st day of the year (2nd in leap years) in the Gregorian calendar. There are 0 days remaining.

Events

  • 553 - The Second Council of Constantinople begins.

..... Click the link for more information.
19th century - 20th century - 21st century
1930s  1940s  1950s  - 1960s -  1970s  1980s  1990s
1958 1959 1960 - 1961 - 1962 1963 1964

Year 1961 (MCMLXI
..... Click the link for more information.
First launched in 1953, the American Redstone rocket was a direct descendant of the German V-2. It was used for the first live nuclear missile tests by the United States. It was also known as the Redstone MRBM (medium range ballistic missile).
..... Click the link for more information.
Cape Canaveral Air Force Station Launch Complex 5 (LC-5) was a Launch Site at Merritt Island, Cape Canaveral, Florida. The site was used for various Redstone and Jupiter launches.
..... Click the link for more information.
Cape Canaveral from the spanish Cabo Cañaveral, is a headland in Brevard County, Florida, United States, near the center of that state's Atlantic coast at and is also 45 minutes East of Orlando by car.
..... Click the link for more information.
A sub-orbital spaceflight (or sub-orbital flight) is a spaceflight in which the spacecraft reaches space, but its trajectory then intersects the atmosphere or surface of the gravitational body from which it was launched, and thus does not enter a stable orbit.
..... Click the link for more information.
Motto
"In God We Trust"   (since 1956)
"E Pluribus Unum"   ("From Many, One"; Latin, traditional)
Anthem
..... Click the link for more information.
Vostok 1
Mission insignia

Mission statistics
Mission name: Vostok 1
Spacecraft name: Ласточка (Lastochka -
Swallow)
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Premier of the Soviet Union is the commonly used English term for the offices of Chairman of the Council of People's Commissars of the USSR (Председатель Совета
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Nikita Sergeyevich Khrushchev (Russian: , Nikita Sergeevič Khruščjov; IPA:
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Vostok 1
Mission insignia

Mission statistics
Mission name: Vostok 1
Spacecraft name: Ласточка (Lastochka -
Swallow)
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Yuri Gagarin
Юрий Гагарин


Cosmonaut
Nationality Russian

Status Deceased
Born March 9 1934
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In office
December 24, 1974–January 6, 1999
Preceded by
Succeeded by



Born July 18 1921 (1921--) (age 86)
Cambridge, Ohio
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First launched in 1953, the American Redstone rocket was a direct descendant of the German V-2. It was used for the first live nuclear missile tests by the United States. It was also known as the Redstone MRBM (medium range ballistic missile).
..... Click the link for more information.
Cape Canaveral from the spanish Cabo Cañaveral, is a headland in Brevard County, Florida, United States, near the center of that state's Atlantic coast at and is also 45 minutes East of Orlando by car.
..... Click the link for more information.
December 9 is the 1st day of the year (2nd in leap years) in the Gregorian calendar. There are 0 days remaining.

Events


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19th century - 20th century - 21st century
1930s  1940s  1950s  - 1960s -  1970s  1980s  1990s
1957 1958 1959 - 1960 - 1961 1962 1963

Year 1960 (MCMLX
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19th century - 20th century - 21st century
1930s  1940s  1950s  - 1960s -  1970s  1980s  1990s
1957 1958 1959 - 1960 - 1961 1962 1963

Year 1960 (MCMLX
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A reaction control system (abbreviated RCS) is a subsystem of a spacecraft. Its purpose is attitude control and steering. An RCS system is capable of providing small amounts of thrust in any desired direction or combination of directions.
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