Mercury Atlas 6
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| Mission Insignia | |
|---|---|
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| Mission Statistics | |
| Mission Name: | Mercury MA-6 |
| Call Sign: | Friendship 7 |
| Number of Crew Members: | 1 |
| Launch: | February 20, 1962 14:47:39 UTC Cape Canaveral Complex 14 |
| Landing: | February 20, 1962 19:43:02 UTC Template:Coor dm |
| Duration: | 4 h 55 min 23 s |
| Number of Orbits: | 3 |
| Distance Traveled: | 75,679 mi 121,794 km |
| Maximum velocity: | 17,544 mph 28,234 km/h |
| Peak acceleration: | 7.7 g (76 m/s²) |
| Mass: | 1,352 kg |
| Crew Picture | |
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| John Glenn | |
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| Contents |
Crew
- John Glenn (flew on Mercury 6 & STS-95)
Backup Crew
Mission Parameters
- Mass: 1,352 kg
- Perigee: 159 km
- Apogee: 265 km
- Inclination: 32.5°
- Period: 88.5 min
See also
Mission Highlights
The Mercury 6 mission was the first attempt by the U.S. and Mercury program to place an astronaut in orbit. The MA-6 mission was launched on February 20, 1962, from Launch Complex 14 at Cape Canaveral, Florida. The flight used Atlas # 109-D and Mercury spacecraft # 13. The spacecraft was named Friendship 7. It made three earth orbits, piloted by astronaut John Glenn, the first American to orbit the Earth.
After the successful completion of the Mercury 5 flight that carried Enos the Chimp in late November, 1961, a press conference was held in early December, 1961. Reporters asked NASA's Robert Gilruth who would be the first U.S. astronaut in orbit, piloting Mercury 6. He then announced the team members for the next two Mercury missions. John H. Glenn was the selected as prime pilot for the first mission (Mercury 6), with M. Scott Carpenter as his backup. Donald K. Slayton and Walter M. Schirra were pilot and backup, respectively, for the second mission, Mercury 7.
The Mercury 6 launch vehicle, Atlas #109-D, arrived at Cape Canaveral the evening of November 30, 1961. NASA had wanted to launch Mercury 6 in 1961 (hoping to orbit an astronaut in the same calendar year as the Soviets did), but by early December it was apparent that the mission hardware would not be ready for launch until early 1962.
Mercury spacecraft # 13, began taking form on the McDonnell, St. Louis, Missouri, assembly line in May, 1960. It was chosen for the MA-6 mission in October, 1960 and delivered to Cape Canaveral on August 27, 1961. Mercury spacecraft # 13 and Atlas # 109-D were stacked on the pad at Launch Complex 14 on January 2, 1962.
The launch date was first announced as January 16, 1962, then postponed to January 23 because of problems with the Atlas rocket fuel tanks. The launch then slipped day by day to January 27 because of weather. On January 27, 1962, John Glenn had been onboard Mercury 6 and ready to launch, when at T-20 minutes, the flight directory called off the launch because of the heavy overcast. The heavy cloud cover would have prevented the necessary photo coverage of the launch.
The launch was postponed until February 1, 1962. When technicians began to fuel the Atlas on January 30, they discovered a fuel leak had soaked an internal insulation blanket between the fuel and oxidizer tanks of the rocket. This caused a two week delay while necessary repairs were made. On February 15, the launch was again postponed due to weather. Finally on February 19, the weather started to break. It appeared that February 20, 1962 would be a favorable day to attempt a launch.
John Glenn boarded the Friendship 7 spacecraft at 11:03 UTC on February 20, 1962. The hatch was bolted in place at 12:10 UTC. Most of the 70 hatch bolts had been secured, when one was discovered to be broken. This caused a 40 minute delay while all the bolts were removed, the defective bolt was replaced and the hatch was re-bolted in place.
At 14:47 UTC, after two hours and 17 minutes of holds and three hours and 44 minutes after Glenn entered Friendship 7, it was finally launched. At liftoff Glenn's pulse rate climbed to 110.
Thirty seconds after liftoff the General Electric-Burroughs guidance system locked onto a radio transponder in the booster to guide the vehicle to orbit. As the Atlas and Friendship 7 passed through max-q Glenn reported, "It's a little bumpy about here." After max-q the flight smoothed out. At two minutes and 14 seconds after launch, the booster engines cut off and dropped away. Then at two minutes and twenty-four seconds, the escape tower was jettisoned, right on schedule.
After the tower was jettisoned, the Atlas and spacecraft pitched over still further, giving Glenn his first view of the horizon. He described the view as "a beautiful sight, looking eastward across the Atlantic." Vibration increased as the last of the fuel supply was used up. At SECO it was found that the Atlas had accelerated the capsule to a velocity only 7 ft/s (2 m/s) below nominal. At 14:52 UTC, Friendship 7 was in orbit. Glenn received word that the Atlas had boosted the MA-6 into a trajectory that would stay up for at least seven orbits. Meanwhile, computers at the Goddard Space Flight Center in Maryland indicated that the MA-6 orbital parameters appeared good enough for almost 100 orbits.
When the posigrade rockets fired and separated the capsule from the booster, the five-second rate-damping operation started two and a half seconds late. This caused a substantial roll error as the capsule began its turnaround. The automatic attitude control system took 38 seconds to place the Friendship 7 into its proper orbital attitude. The turnaround maneuver used 5.4 pounds (2.4 kg) of fuel from a total supply of 60.4 pounds (27.4 kg) (36 lb (16.3 kg) for automatic and 24.4 lb (11.1 kg) for manual control system). The spacecraft then settled into orbital flight with a velocity of 17,544 mph (7,843 m/s).
Friendship 7 began its first orbit with all systems go. It crossed the Atlantic and passed over the Canary Islands. Controllers there reported all capsule systems in perfect working order. Looking at the African coastline, and later the interior over Kano, Nigeria, Glenn told the tracking station team that he could see a dust storm. Kano flight communicators replied that the winds had been quite heavy for the past week.
Over Kano, Nigeria, Glenn took control of the spacecraft and started a major yaw adjustment. He allowed the spacecraft to continue the yaw maneuver until it was facing into its flight path. Glenn noticed that the attitude indicators disagreed with what he observed were the true spacecraft attitudes. Even with the incorrect instrument readouts, he was pleased to be facing the forward instead of backward on his orbital path.
Over the Indian Ocean on his first orbit, Glenn observed his first sunset from orbit. He described the moment of twilight as "beautiful." Space sky was very black, he said, with a thin band of blue along the horizon. Glenn described the sunset. The sun went down fast but not as quickly as he had expected. For five or six minutes there was a slow reduction in light intensity. Brilliant orange and blue layers spread out 45 to 60 degrees on either side of the sun, tapering gradually toward the horizon. Clouds prevented him from seeing a mortar flare fired by the Indian Ocean tracking ship as part of a pilot observation experiment.
Continuing his journey on the night side of Earth, nearing the Australian coastline, Glenn made star, weather, and landmark observations. He failed to see the dim light phenomenon known as zodiacal light. His eyes had not had sufficient time to adapt to the darkness.
The spacecraft came into radio range of Muchea, Australia. At the Mercury Tracking Station there, Gordon Cooper was the capsule communicator. Glenn reported that he felt fine and had no problems. He saw a very bright light and what appeared to be the outline of a city. Cooper said that he probably was looking at the lights of Perth and Rockingham. "That sure was a short day," he excitedly told Cooper. "That was about the shortest day I've ever run into."
The spacecraft moved across Australia and across the Pacific to Canton Island. Glenn experienced a short 45 minute night and prepared the periscope for viewing his first sunrise in orbit. As the sun rose over Canton Island, he saw thousands of "little specks, brilliant specks, floating around outside the capsule." Glenn had the impression that the spacecraft was tumbling or that he was looking into a star field. A quick hard look out of the spacecraft window corrected this momentary illusion. He definitely thought the "fireflies," as he called the small objects, were streaming past his spacecraft from ahead. They seemed to flow by slowly but did not seem to be coming from any part of the spacecraft. As Friendship 7 moved into brighter sunlight, the "fireflies" disappeared. They were probably small ice crystals venting from onboard spacecraft systems.
As the spacecraft crossed the Kauai, Hawaii tracking station, Glenn noticed a lot of interference on the HF radio band. As he crossed the Pacific coast of North America the tracking station at Guaymas, Mexico, informed Mercury Control in Florida that a yaw thruster was causing attitude control problems. Glenn later recalled, this problem "was to stick with me for the rest of the flight."
Glenn noticed the control problem when the automatic stabilization and control system allowed the spacecraft to drift about a degree and a half per second to the right. Glenn switched control to manual-proportional control mode and moved Friendship 7 back to the proper attitude. He tried different control modes to see which used the least fuel to maintain attitude. The manual fly-by-wire combination used the least fuel. After about twenty minutes the yaw thruster began working again and Glenn switched back to the automatic control system. It worked for a short time and then began having problems again, this time with the opposite yaw thruster. He then switched back to the manual fly-by-wire system and flew the spacecraft in that mode for the remainder of the flight.
As Friendship 7 crossed Cape Canaveral at the start of its second orbit, a flight controller noticed that "Segment 51", an sensor providing data on the spacecraft landing system, was giving a strange reading. According to the reading, the heat shield and landing bag were no longer locked in position. If this were the case, the heat shield was only being held against the spacecraft by the straps of the retro package. Mercury Control ordered all tracking sites to monitor "Segment 51" closely and advise Glenn that the landing-bag deploy switch should be in the "off" position.
Glenn was not immediately aware of the problem, but he became suspicious when site after site asked him to make sure that the landing-bag deploy switch was off. Meanwhile Friendship 7 was crossing the Atlantic for the second time. Glenn was busy manually keeping the spacecraft attitude correct and also trying to accomplish as many of the flight plan tasks as he could.
Crossing over the Canary Islands, Glenn observed that the "fireflies" outside the spacecraft had no connection with gas from the reaction control jets. His suit temperature felt too warm, but he didn't take time to adjust it. The Kano, Nigeria and Zanzibar sites suddenly noticed a 12 percent drop in the spacecraft secondary oxygen supply.
During his second pass over the Indian Ocean, Glenn found that the Indian Ocean tracking ship was in heavy weather. Instead of releasing balloons for a pilot observation experiment, the ship fired star-shell parachute flares as Friendship 7 passed overhead. Glenn only was able to observe the flashes of lightning from storms in the area.
The temperature in Glenn's spacesuit was too warm. It had been since he passed over the Canary Islands, earlier in the second orbit. As he crossed the Indian Ocean he tried to adjust the suit temperature. Coming up on Woomera, Australia, a signal light came on warning him of excess cabin humidity. For the rest of the flight Glenn had to carefully balance suit cooling against the cabin humidity.
While still over Australia, another warning light came on, indicating that the fuel supply for the automatic control system was down to 62 percent. Mercury Control recommended that Glenn let the spacecraft attitude drift to conserve fuel.
There were no more problems for Friendship 7 during the remainder of the second orbit. He continued to manually control the spacecraft attitude, not allowing it too drift too far out of alignment. In doing so, he consumed more fuel than a functioning automatic system would have used. Fuel consumption was 6 pounds (2.7 kg) from the automatic tank and 11.8 pounds (5.4 kg) from the manual tank, during the second orbit. This amounted to almost 30 percent of the total fuel supply.
On the third orbit of Friendship 7, the Indian Ocean tracking ship did not attempt to launch any objects for pilot observation experiments. The cloud coverage was still too thick. When the spacecraft came across Australia for the third time, Glenn joked with Cooper at the Muchea Tracking Station. The Glenn jokingly asked Cooper to notify General Shoup, Commandant of the Marine Corps, that three orbits should meet the minimum monthly requirement of four hours' flying time. He also asked to be certified as eligible for his regular flight pay.
Meanwhile, Mercury Control had been monitoring the "Segment 51", situation. The Hawaiian tracking station asked Glenn to toggle the landing bag deploy switch into the automatic position. If a light came on, reentry should take place while retaining the retro pack. Adding this to past questions about the landing bag switch, Glenn realized there was a possible problem with a loose heat shield. The test was run but no light appeared. Glenn also reported there were no bumping noises during spacecraft maneuvers.
Mercury Control was still undecided on the course of action to take. Some controllers thought the retro pack should be jettisoned after retrofire, while other controllers thought the retro pack should be retained, as added assurance that the heat shield would stay in place.
Flight Director Christopher Kraft and Mission Director Walter C. Williams, decided to keep the retro pack in place during reentry. Walter Schirra, the California communicator at Point Arguello, relayed the instructions to Glenn. The retro pack should be retained until the spacecraft was over the Texas tracking station.
Glenn was now preparing for reentry. Retaining the retro package would mean, he had to retract the periscope manually. He would also have to activate the .05-g sequence by pushing the override switch. Friendship 7 neared the California coast. It had been four hours and 33 minutes since launch. The spacecraft was maneuvered into retrofire attitude and the first retrorocket fired. "Boy, feels like I'm going halfway back to Hawaii," Glenn radioed. The second and then the third retros fired at five second intervals. The spacecraft attitude was steady during retrofire. Six minutes after retrofire; Glenn maneuvered the spacecraft into a 14 degree nose up, pitch attitude for reentry.
Friendship 7 lost altitude in its reentry glide over the continental United States, headed toward splashdown in the Atlantic. The Texas tracking station told Glenn to retain the retro pack until the accelerometer read 1.5 g (14.7 m/s²). Glenn reported as he crossed Cape Canaveral he had been controlling the spacecraft manually and would use the fly-by–wire mode as a backup. Mercury Control then gave him the 0.05 g (0.49 m/s²) mark, and he pressed the override button. About the same time, Glenn heard noises that sounded like "small things brushing against the capsule." "That's a real fireball outside," he radioed Mercury Control. A strap from the retro package broke partially loose and hung over the spacecraft window as it was consumed in the reentry plasma stream. The spacecraft control system was working well but the manual fuel supply was down to 15 percent. The peak of reentry deceleration was still to come. Glenn switched to fly-by-wire and the automatic tank supply. This combination had more available fuel.
The spacecraft now experienced peak reentry heating. Glenn later reported, "I thought the retro pack had jettisoned and saw chunks coming off and flying by the window." He feared the chunks were pieces of his heatshield that might be disintegrating. The chunks were pieces of the retro package breaking up in the reentry fireball.
After passing the peak g region, the Friendship 7 began oscillating severely. The astronaut could not control the ship manually. The spacecraft was oscillating past 10 degrees on both sides of the vertical zero-degree point. "I felt like a falling leaf," Glenn later said. He activated the auxiliary damping system, this helped stabilize the large yaw and roll rates. Fuel in the automatic tanks was getting low. Glenn wondered if the spacecraft would retain stability until it was low enough to deploy the drogue parachute.
The automatic fuel supply ran out at 1 minute and 51 seconds, and manual fuel ran out at 51 seconds, before drogue chute deployment. The oscillations resumed, at 35,000 feet (10 km) Glenn decided to deploy the drogue chute manually to regain attitude stability. Just before he reached the switch, the drogue chute opened automatically at 28,000 feet (8.5 km) instead of the programmed 21,000 feet (6.4 km). The spacecraft regained stability and Glenn reported, "everything was in good shape."
At 17,000 feet (5 km) the periscope opened and was available for the astronaut to use. Glenn tried to look out the overhead window instead, but it was coated with so much smoke and film that he could see very little. The spacecraft continued to descend on the drogue chute. The antenna section jettisoned and the main chute deployed and opened to its full diameter. Mercury Control reminded Glenn to manually deploy the landing bag. He toggled the switch and the green light confirmation came on. A "clunk" could be heard as the heat shield and landing bag dropped into place, four feet (1.2 m) below the capsule.
Friendship 7 had splashed down in the Atlantic about 40 miles (60 km) short of the planned landing zone. Retrofire calculations had not taken into account spacecraft weight loss due to use of onboard consumables. The USS Noa, a destroyer code-named Steelhead, had spotted the spacecraft when it was descending on its parachute. The destroyer was about six miles (10 km) away when it radioed Glenn that it would reach him shortly. The Noa came alongside Friendship 7 seventeen minutes later.
One crewman cleared the spacecraft antenna and another crewman attached a line to hoist Friendship 7 aboard. After being pulled from the water the spacecraft bumped against the side of the destroyer. Once Friendship 7 was on deck, Glenn intended to leave the capsule through the upper hatch. But it was too hot in the spacecraft and Glenn decided to blow the side hatch instead. He told the ship's crew to stand clear and hit the hatch detonator plunger with the back of his hand. The detonator plunger recoiled, and slightly cut the astronauts knuckles through his glove. With a loud bang, the hatch was off. A smiling John Glenn got out of Friendship 7 and stood on the deck of the Noa. His first words were, "It was hot in there."
According to a chart printed in the NASA publication, "Results of the First United States Manned Orbital Space Flight, Feb. 20, 1962", the landing coordinates are near Template:Coor dm.
The astronaut and spacecraft came through the mission in good shape. America had taken its first step on the way to the moon.
The "Segment 51" warning light problem was later determined to be a faulty sensor switch. The heat shield and landing bag were in fact secure during reentry.
February 21, 1962, a metal fragment was recovered on a farm in South Africa. It was identified as coming from the MA-6 Atlas launch vehicle by numbers stamped on it. The fragment had landed on the farm after about 8 hours in orbit.
Mercury spacecraft # 13 - Friendship 7, used in the Mercury-Atlas 6 mission, is currently displayed at the National Air and Space Museum, Washington D.C. Mercury spacecraft #13 Friendship 7 display page on A Field Guide to American Spacecraft website. (http://aesp.nasa.okstate.edu/fieldguide/pages/mercury/ma-6.html)
Mercury-Atlas Three Orbit Flight Events
| T+ Time | Event | Description |
|---|---|---|
| T+00:00:00 | Liftoff | Mercury-Atlas lifts off, onboard clock starts. |
| T+00:00:02 | Roll Program | Mercury-Atlas rotates along its axis 2.5 deg/s from 30 to 0 deg. |
| T+00:00:16 | Pitch Program | Mercury-Atlas begins a 0.5 deg/s pitch from 90 to 0 deg. |
| T+00:00:30 | Radio Guidance Lock | General Electric-Burroughs guidance system locks onto radio transponder in Atlas booster to guide the vehicle until orbit insertion. |
| T+00:01:24 | Max Q | Maximum dynamic pressure 980 lbf/ft² (6.75 MPa) |
| T+00:02:10 | BECO | Atlas Booster Engine Cutoff. Booster engines drop away. |
| T+00:02:33 | Tower Jettison | Escape Tower Jettison, no longer needed. |
| T+00:02:25 | Atlas Pitchover | After tower separation, vehicle pitches over further. |
| T+00:05:20 | SECO | Atlas Sustainer Engine Cutoff, capsule reaches orbit, velocity 17,547 mph (7,844 m/s) |
| T+00:05:24 | Capsule Separation | Posigrade rockets fire for 1 s giving 15 ft/s (4.57 m/s) separation. |
| T+00:05:25 | 5 second Rate Damping | ASCS damps capsule rates for 5 seconds in preparation for turnaround maneuver. |
| T+00:05:25 | Turnaround Maneuver | Capsule (ASCS) system rotates capsule 180 degrees, to heat shield forward attitude. Nose is pitched down 34 degrees to retro fire position. |
| T+00:05:30 T+04:30:00 | Orbital Operations | Orbital operations and experiments for 3 orbits. |
| T+04:30:00 | Retro Sequence Start | Retrofire in 30 s. (ASCS) checks for proper retro attitude -34 deg pitch, 0 deg yaw, 0 deg roll. |
| T+04:30:30 | Retrofire | Three retro rockets fire for 10 seconds each. They are started at 5 second intervals, firing overlaps for a total of 20 s. Delta V of 550 ft/s (168 m/s) is taken off forward velocity. |
| T+04:35:45 | Retract Periscope | Periscope is automatically retracted in preparation for reentry. |
| T+04:36:15 | Retro Pack Jettison | One minute after retrofire retro pack is jettisoned, leaving heatshield clear. |
| T+04:36:20 | Retro Attitude Maneuver | (ASCS) orients capsule in 34 degres nose down pitch, 0 degrees roll, 0 degrees yaw. |
| T+04:42:15 | .05 G Maneuver | (ASCS) detects beginning of reentry and rolls capsule at 10 deg/s to stabilize capsule during reentry. |
| T+04:49:38 | Drogue Parachute Deploy | Drogue parachute deployed at 22,000 ft (6.7 km) slowing descent to 365 ft/s (111 m/s) and stabilizing capsule. |
| T+04:49:45 | Snorkel Deploy | Fresh air snorkel deploys at 20,000 ft (6 km) ECS switches to emergency oxygen rate to cool cabin. |
| T+04:50:15 | Main Parachute Deploy | Main parachute deploys at 10,000 ft (3 km). Descent rate slows to 30 ft/s (9 m/s) |
| T+04:50:20 | Landing Bag Deploy | Landing Bag Deploys, dropping heat shield down 4 ft (1.2 m). |
| T+04:50:20 | Fuel Dump | Remaining hydrogen peroxide fuel automatically dumped. |
| T+04:55:30 | Splashdown | Capsule lands in water about 500 mi (800 km) downrange from launch site. |
| T+04:55:30 | Rescue Aids Deploy | Rescue aid package deployed. The package includes green dye marker, recovery radio beacon and whip antenna. |
Reference
- This New Ocean: A History of Project Mercury - NASA SP-4201 (http://www.hq.nasa.gov/office/pao/History/SP-4201/cover.htm)
- NASA NSSDC Master Catalog (http://nssdc.gsfc.nasa.gov/nmc/sc-query.html)
- Results of the first US manned orbital space flight - Feb 20, 1962 (Friendship 7) NASA report - (PDF format) (http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930074071_1993074071.pdf)
- This New Ocean: A History of Project Mercury - NASA report (PDF format) (http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19990026158_1999028570.pdf)
- Chronology of Project Mercury - NASA report (PDF format) (http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19630011968_1963011968.pdf)
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