| McDonnell Mercury capsule | ||
|---|---|---|
| Description | ||
| Role: | Suborbital and orbital spaceflight | |
| Crew: | one, pilot | |
| Dimensions | ||
| Height: | 11.5 ft | 3.51 m |
| Diameter: | 6.2 ft | 1.89 m |
| Volume: | 60 ft3 | 1.7 m3 |
| Weights (MA-6) | ||
| Launch: | 4,265 lb | 1,935 kg |
| Orbit: | 2,986 lb | 1,354 kg |
| Post Retro: | 2,815 lb | 1,277 kg |
| Reentry: | 2,698 lb | 1,224 kg |
| Landing: | 2,421 lb | 1,098 kg |
| Rocket engines | ||
| Retros (solid fuel) x 3: | 1,000 lbf ea | 4.5 kN |
| Posigrade (solid fuel) x 3: | 400 lbf ea | 1.8 kN |
| RCS high (H2O2) x 6: | 25 lbf ea | 108 N |
| RCS low (H2O2) x 6: | 12 lbf ea | 49 N |
| Performance | ||
| Endurance: | 34 hours | 22 orbits |
| Apogee: | 175 miles | 282 km |
| Perigee: | 100 miles | 160 km |
| Retro delta v: | 300 mph | 483 km/h |
| Mercury capsule diagram | ||
| McDonnell Mercury capsule | ||
Project Mercury was the United States' first successful manned spaceflight program. It ran from 1959 through 1963 with the goal of putting a man in orbit around the Earth. Early planning and research was carried out by NACA, while the program was officially carried out by the newly created NASA. The name comes from Mercury, a Roman mythological god who is often seen as a symbol of speed. Mercury is also the name of the innermost planet of the solar system, which revolves around the sun faster than any other, hence the image of speed, although Project Mercury had no other connection to that planet.
The Mercury program cost $1.5 billion. See NASA Budget.
During the launch phase of the mission, the Mercury spacecraft and astronaut were protected from launch vehicle failures by the Launch Escape System. The LES consisted of a solid fuel, 52,000 lbf (231 kN) thrust rocket mounted on a tower above the spacecraft. In the event of a launch abort, the LES fired for 1 second, pulling the Mercury spacecraft away from a defective launch vehicle. The spacecraft would then descend on its parachute recovery system. After booster engine cutoff (BECO), the LES was no longer needed and was separated from the spacecraft by a solid fuel, 800 lbf (3.6 kN) thrust jettison rocket that fired for 1.5 seconds.
To separate the Mercury spacecraft from the launch vehicle, the spacecraft fired three small solid-fuel, 400 lbf (1.8 kN) thrust rockets for 1 second. These rockets are called the Posigrade rockets.
The spacecraft was only equipped with attitude control thrusters - after orbit insertion and before retrofire they could not change their orbit. There were three sets of high and low powered automatic control jets and separate manual jets - one for each axis (yaw, pitch and roll), supplied from two separate fuel tanks - one automatic and one manual. The pilot could use any one of the three thruster systems and fuel them from either of the two fuel tanks to provide spacecraft attitude control.
The Mercury spacecraft were designed to be totally controllable from the ground in the event that the space environment impaired the pilot's ability to function.
The spacecraft had three solid-fuel, 1000 lbf (4.5 kN) thrust retrorockets that fired for 10 seconds each. One was sufficient to return the spacecraft to earth if the other two failed. The firing sequence (known as ripple firing) required firing the first retro, followed by the second retro five seconds later (while the first was still firing). Five seconds after that, the third retro fired (while the second retro was still firing).
There was a small metal flap at the nose of the spacecraft called the "spoiler". If the spacecraft started to reenter nose first (another stable reentry attitude for the capsule), airflow over the "spoiler" would flip the spacecraft around to the proper, heatshield-first reentry attitude. During reentry, the astronaut would experience about 4 g-forces.
Initial designs for the spacecraft suggested the use of either beryllium heat-sink heat shields or an ablative shield. Extensive testing settled the issue - ablative shields proved to be reliable (so much so that the initial shield thickness was safely reduced, allowing a lower total spacecraft weight), easier to produce (at that time, beryllium was only produced in sufficient quantities by a single company in the US) and cheaper.
NASA ordered 20 production spacecraft, numbered 1 through 20, from McDonnell Aircraft Company, St. Louis, Missouri. Five of the twenty spacecraft were not flown. They were Spacecraft #10, 12, 15, 17, and 19. Two unmanned spacecraft were destroyed during flights. They were Spacecraft #3 and #4. Spacecraft #11 sank and was recovered from the bottom of the Atlantic Ocean after 38 years. Some spacecraft were modified after initial production (refurbished after launch abort, modified for longer missions, etc) and received a letter designation after their number, examples 2B, 15B. Some spacecraft were modified twice; for example, spacecraft 15 became 15A and then 15B.
A number of boilerplate spacecraft (mockup/prototype/replica spacecraft, made from non-flight materials or lacking production spacecraft systems and/or hardware) were also made by NASA and McDonnell Aircraft and used in numerous tests, including launches.
Little Joe was used to test the escape tower and abort procedures. Redstone was used for suborbital flights, and Atlas for orbital ones. Starting in October, 1958, Jupiter missiles were also considered as suborbital launch vehicles for the Mercury program, but were cut from the program in July, 1959 due to budget constraints. The Atlas boosters required extra strengthening in order to handle the increased weight of the Mercury capsules beyond that of the nuclear warheads they were designed to carry. Little Joe was a solid-propellant booster designed specially for the Mercury program.
The Titan missile was also considered for use for later Mercury missions, however the Mercury program was terminated before these missions were flown. The Titan was used for the Gemini program which followed Mercury.
| Mission | Rocket | Call Sign | Launch Date | Launch Time | Duration | Remarks |
|---|---|---|---|---|---|---|
| Mercury-Jupiter | Jupiter (missile) | N/A | N/A | N/A | N/A | Cancelled in July, 1959 - Proposed suborbital launch vehicle for Mercury. Not flown. |
| Little Joe 1 | Little Joe | LJ-1 | August 21, 1959 | N/A | 00d 00h 00 m 20s | Test of launch escape system during flight. |
| Big Joe 1 | Atlas 10-D | Big Joe 1 | September 9, 1959 | N/A | 00d 00h 13 m | Test of heat shield and Atlas / spacecraft interface. |
| Little Joe 6 | Little Joe | LJ-6 | October 4, 1959 | N/A | 00d 00h 05 m 10s | Test of capsule aerodynamics and integrity. |
| Little Joe 1A | Little Joe | LJ-1A | November 4, 1959 | N/A | 00d 00h 08 m 11s | Test of launch escape system during flight. |
| Little Joe 2 | Little Joe | LJ-2 | December 4, 1959 | N/A | 00d 00h 11 m 06s | Carried Sam the monkey to 85 kilometres in altitude. |
| Little Joe 1B | Little Joe | LJ-1B | January 21, 1960 | N/A | 00d 00h 08 m 35s | Carried Miss Sam the monkey to 9.3 statute miles (15 kilometres) in altitude. |
| Beach Abort | Launch escape system | Beach Abort | May 9, 1960 | N/A | 00d 00h 01 m 31s | Test of the Off-The-Pad abort system. |
| Mercury-Atlas 1 | Atlas | MA-1 | July 29, 1960 | 13:13 UTC | 00d 00h 03 m 18s | First flight of Mercury spacecraft and Atlas Booster. |
| Little Joe 5 | Little Joe | LJ-5 | November 8, 1960 | N/A | 00d 00h 02 m 22s | First flight of a production Mercury spacecraft. |
| Mercury-Redstone 1 | Redstone | MR-1 | November 21, 1960 | N/A | 00d 00h 00 m 02s | Launched 4 inches (100 mm). Settled back on pad due to electrical malfunction. |
| Mercury-Redstone 1A | Redstone | MR-1A | December 19, 1960 | N/A | 00d 00h 15 m 45s | First flight of Mercury spacecraft and Redstone booster. |
| Mercury-Redstone 2 | Redstone | MR-2 | January 31, 1961 | 16:55 UTC | 00d 00h 16 m 39s | Carried Ham the Chimpanzee on suborbital flight. |
| Mercury-Atlas 2 | Atlas | MA-2 | February 21, 1961 | 14:10 UTC | 00d 00h 17 m 56s | Test of Mercury spacecraft and Atlas Booster. |
| Little Joe 5A | Little Joe | LJ-5A | March 18, 1961 | N/A | 00d 00h 23 m 48s | Test of the launch escape system during the most severe conditions of a launch. |
| Mercury-Redstone BD | Redstone | MR-BD | March 24, 1961 | 17:30 UTC | 00d 00h 8 m 23s | Redstone Booster Development - test flight. |
| Mercury-Atlas 3 | Atlas | MA-3 | April 25, 1961 | 16:15 UTC | 00d 00h 07 m 19s | Test of Mercury spacecraft and Atlas Booster. |
| Little Joe 5B | Little Joe | AB-1 | April 28, 1961 | N/A | 00d 00h 05 m 25s | Test of the launch escape system during the most severe conditions of a launch. |
| Mercury-Atlas 4 | Atlas | MA-4 | September 13, 1961 | 14:09 UTC | 00d 01h 49 m 20s | Test of Mercury spacecraft and Atlas Booster. Completed 1 orbit. |
| Mercury-Scout 1 | Scout | MS-1 | November 1, 1961 | 15:32 UTC | 00d 00h 00 m 44s | Test of Mercury tracking network. |
| Mercury-Atlas 5 | Atlas | MA-5 | November 29, 1961 | 15:08 UTC | 00d 03h 20 m 59s | Carried Enos the Chimpanzee on a two orbit flight. |
Mercury had seven prime astronauts, all former military test pilots, known as the Mercury Seven. NASA announced the selection of these astronauts on April 9, 1959.
| Mission | Rocket | Designation | Pilot | Launch Date | Launch Time | Duration | Remarks |
|---|---|---|---|---|---|---|---|
| Mercury-Redstone 3 | Redstone | MR-3 | Shepard | May 5, 1961 | 14:34 UTC | 00d 00h 15 m 28s | Capsule call sign "Freedom 7". First American to make a suborbital flight into space. |
| Mercury-Redstone 4 | Redstone | MR-4 | Grissom | July 21, 1961 | 12:20 UTC | 00d 00h 15 m 37s | "Liberty Bell 7". Second suborbital flight. Capsule sank before recovery when hatch unexpectedly blew off. |
| Mercury-Atlas 6 | Atlas | MA-6 | Glenn | February 20, 1962 | 14:47 UTC | 00d 04h 55 m 23s | "Friendship 7". First American to orbit the Earth (for a total of 3 orbits). Capsule's retropack retained during re-entry due to concerns about heatshield. |
| Mercury-Atlas 7 | Atlas | MA-7 | Carpenter | May 24, 1962 | 12:45 UTC | 00d 04h 56 m 15s | "Aurora 7". 3 orbits. Reentered off-target by 402 km. Pilot Carpenter replaced Deke Slayton. |
| Mercury-Atlas 8 | Atlas | MA-8 | Schirra | October 3, 1962 | 12:15 UTC | 00d 09h 13 m 11s | "Sigma 7". Carried out engineering tests. 6 orbits. |
| Mercury-Atlas 9 | Atlas | MA-9 | Cooper | May 15, 1963 | 13:04 UTC | 01d 10h 19 m 49s | "Faith 7". First American in space for over a day. 22 orbits. |
| Mercury 10 | Atlas | MA-10 | Shepard | N/A | N/A | N/A | "Freedom 7-II". Intended to be a 3-day mission in October, 1963. Cancelled June 13, 1963. |
Flight patches that purport to be patches from various Mercury missions are available to the public. In reality, these patches were designed by private entrepreneurs long after the Mercury program ended. When genuine flight patches were created by crews in the Gemini program, this caused a public demand for Mercury flight patches, which was filled by these private entrepreneurs. The only patches the Mercury astronauts wore were the NASA logo and a name tag. Each manned Mercury spacecraft, however, was decorated with a flight insignia. These are the genuine Mercury flight insignias.
The names of five of the Mercury astronauts are also commemorated in the popular 1960s TV show Thunderbirds. In the series, Jeff Tracy, the founder of the fictional International Rescue organisation, is a millionaire ex-astronaut who has named his five sons -- Scott, Virgil, Alan, John and Gordon -- after the real-life Mercury astronauts.
Manned spacecraft | Mercury program
Mercury-Programm | Proyecto Mercury | Programme Mercury | Programma Mercury | תוכנית מרקורי | Mercury Programm | Mercury | マーキュリー計画 | Program Mercury | Projeto Mercury | Меркурий (космическая программа) | Program Mercury | Mercuryprogrammet
This article is licensed under the GNU Free Documentation License.
It uses material from the
"Project Mercury".
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