Mercury-Atlas 7

"Mercury 7" redirects here. For the group of astronauts, see Mercury Seven.

Mercury-Atlas 7
Mission insignia
Mission statistics
Mission name	Mercury-Atlas 7
Spacecraft name	Aurora 7
Spacecraft mass	1,350.0 kilograms (2,976 lb)
Crew size	1
Call sign	Aurora 7
Launch vehicle	Atlas LV-3B
Launch pad	LC-14 (CCAFS)
Launch date	May 24, 1962 12:45:16 UTC
Landing	May 24, 1962 17:41:21 UTC
Mission duration	04:56:05
Number of orbits	3
Apogee	260 kilometres (140 nmi)
Perigee	154 kilometres (83 nmi)
Orbital period	88.3 min.
Orbital inclination	32.5°
Distance traveled	122,344 kilometres (76,021 mi)
Maximum velocity	28,242 kilometres per hour (17,549 mph)
Peak acceleration	7.8 g (76 m/s²)
Crew photo
Malcolm Scott Carpenter
Related missions
Previous mission Subsequent mission MA-6 MA-8

Mercury-Atlas 7 was the second American orbital Mercury program manned space mission, launched May 24, 1962. The Mercury spacecraft was named Aurora 7 and made three Earth orbits, piloted by astronaut Scott Carpenter. A targeting mishap during reentry took the spacecraft 250 miles (about 400 km) off course, delaying recovery of Carpenter and the craft. The mission used Mercury spacecraft No. 18 and Atlas launch vehicle No. 107-D.

Crew

Position	Astronaut
Pilot	M. Scott Carpenter First spaceflight

Backup crew

Position	Astronaut
Pilot	Walter M. Schirra

Crew notes

The original prime crew for Mercury Atlas-7 was to have been Deke Slayton, with Schirra as his back-up. However Slayton was removed from all flight crew availability after the discovery of cardiac arrhythmia during a training run in the g-loading centrifuge. If Slayton had flown MA-7, his spacecraft would have been named Delta 7, as this would have been the fourth manned flight and Delta (Δ) is the fourth letter in the Greek alphabet.^{[clarification needed]}

Mission parameters

• Mass: 2975 lb (1350 kg)
• Perigee: 154 km
• Apogee: 260 km
• Inclination: 32.5°
• Period: 88.3 min

Mission highlights

Mercury spacecraft No. 18 was delivered to Cape Canaveral, Florida on November 15, 1961. Atlas No. 107-D was rolled out of the Convair factory in San Diego, California on February 25, 1962. It was delivered to Cape Canaveral on March 6, 1962.

MA-7 launch

The focus of Carpenter's five-hour mission was on science. The full flight plan included the first study of liquids in weightlessness, Earth photography and an unsuccessful attempt to observe a flare fired from the ground. At dawn of the third and final orbit, Carpenter inadvertently bumped his hand against the inside wall of the cabin and solved a mystery from the previous flight. The resulting bright shower of particles outside the spacecraft - what John Glenn had called "fireflies" - turned out to be ice particles shaken loose from the spacecraft's exterior.

Like Glenn, Carpenter circled the Earth three times. Total time weightless 4 h 39 min 32 s. The performance of the Mercury spacecraft and Atlas launch vehicle was excellent in nearly every respect. All primary mission objectives were achieved. The single mission-critical malfunction which occurred involved a failure in the spacecraft pitch horizon scanner, a component of the automatic control system. This anomaly was adequately compensated for by the pilot in subsequent in-flight operations so that the success of the mission was not compromised. A modification of the spacecraft control-system thrust units was effective. Cabin and pressure-suit temperatures were high but not intolerable. Some uncertainties in the data telemetered from the bioinstrumentation prevailed at times during the flight; however, associated information was available which indicated continued well-being of the astronaut.

Equipment was included in the spacecraft which provided valuable scientific information; notably that regarding liquid behavior in a weightless state, identification of the airglow layer observed by Astronaut Glenn, and photography of terrestrial features and meteorological phenomena. An experiment which was to provide atmospheric drag and color visibility data in space through deployment of an inflatable sphere was partially successful. The flight further qualified the Mercury spacecraft systems for manned orbital operations and provided evidence for progressing into missions of extended duration and consequently more demanding systems requirements.

Partly because he had been distracted watching the fireflies and partly because of his busy schedule, and a malfunction of the automatic alignment system, Carpenter overshot his planned reentry mark and splashed down 402 kilometers from target.

Aurora 7 is displayed at the Museum of Science and Industry in Chicago, Illinois.^[1]

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°.
T+00:00:16	Pitch Program	Mercury-Atlas begins a 0.5 deg/s pitch from 90° to 0°.
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 (47 kPa)
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, spacecraft reaches orbit, velocity 17,547 mph (7,844 m/s).
T+00:05:24	Spacecraft Separation	Posigrade rockets fire for 1 second giving 15 ft/s (5 m/s) separation.
T+00:05:25	5-Second Rate Damping	ASCS damps spacecraft rates for 5 seconds in preparation for turnaround maneuver.
T+00:05:25	Turnaround Maneuver	Spacecraft (ASCS) system rotates spacecraft 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° pitch, 0° yaw, 0° 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 seconds. Delta V of 550 ft/s (168 m/s) is taken off forward velocity.
T+04:31:00	Retract Periscope	Periscope is automatically retracted in preparation for reentry.
T+04:31:50	Retro Pack Jettison	One minute after retrofire retro pack is jettisoned, leaving heatshield clear.
T+04:33:00	Retro Attitude Maneuver	(ASCS) orients spacecraft in 34° nose down pitch, 0° roll, 0° yaw.
T+04:40:30	0.05 G Maneuver	(ASCS) detects beginning of reentry and rolls spacecraft at 10 degrees per second to stabilize spacecraft during reentry.
T+04:50:20	Drogue Parachute Deploy	Drogue parachute deployed at 22,000 ft (6.7 km) slowing descent to 365 ft/s (111 m/s) and stabilizing spacecraft.
T+04:50:25	Snorkel Deploy	Fresh air snorkel deploys at 20,000 ft (6 km) ECS switches to emergency oxygen rate to cool cabin.
T+04:51:55	Main Parachute Deploy	Main parachute deploys at 10,000 ft (3 km). Descent rate slows to 30 ft/s (9 m/s).
T+04:52:00	Landing Bag Deploy	Landing Bag Deploys, dropping heat shield down four feet (1.2 m).
T+04:52:30	Fuel Dump	Remaining hydrogen peroxide fuel automatically dumped.
T+04:57:10	Splashdown	Spacecraft lands in water.
T+04:57:10	Rescue Aids Deploy	Rescue aid package deployed. The package includes green dye marker, recovery radio beacon and whip antenna.

See also

• Splashdown

References

1. ^ "Mercury MA-7". Encyclopedia Astronautica. http://www.astronautix.com/flights/merryma7.htm. Retrieved 2008-03-13. 

External links

• Results of the Second U.S. Manned Orbital Space Flight, May 24, 1962 NASA report - (PDF format)
• This New Ocean: A History of Project Mercury - NASA report (PDF format)
• Project Mercury: A Chronology - NASA report (PDF format)
• NASA NSSDC Spacecraft Details