Everything you never knew you wanted to know about the Mercury Project

Mercury development chronology

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1959

January 1959

February 1959

March 1959

12 March 1959 
Mercury Manned Orbital Capsule Detailed Specification issued

April 1959

Drop tests showed that the original extended-skirt main parachute was unreliable for operation at altitudes of 10,000 feet and was replaced by a 'ring-sail' parachute of similar size. In at least one drop test the main parachute failed to open and assumed a 'squidding' condition.

9-10 April 1959 
Static stability and drag characteristics of two different escape configurations for the Mercury spacecraft were assessed at the Arnold Engineering Development Center, Tullahoma, Tennessee.
10 April 1959 
Tests of canting angles for the escape motor were conducted at Wallops Island. Angles between 10 and 30 degrees in increments of 5 degrees were tested. Stability appeared to increase with larger angles.
10 April 1959 
Mercury Manned Orbital Capsule Detailed Specification revised
12 April 1959 
The second of the beach abort tests with full scale model completed at Wallops Island
12 April 1959 
Langley was conducting tests of an aluminum honeycomb structure to absorb the loads of landing impact.
13 April 1959 
Tests of small scale models of the spacecraft and escape tower combination were tested at Wallops Island. The next day a full scale model was launched. Escape motor firing, tower jettison, parachute deployment and recovery via helicopter were successfully demonstrated.
22 April 1959 
The escape tower was chosen as the best configuration for the Mercury escape system at a meeting at Langley
27 April 1959 
Project Mercury was granted DX procurement priority.

May 1959

June 1959

July 1959

15 July 1959 
Mercury Manned Orbital Capsule Detailed Specification revised
22 July 1959 
First beach abort test using Mercury boilerplate spacecraft
22 July 1959 
Second beach abort test using Mercury boilerplate spacecraft

August 1959

August 21, 1959 
LJ-1 launched from Wallops Island
September 9, 1959 
BJ-1 launched from Cape Canaveral

September 1959

9/9/59 Big Joe Launch
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9/9/59 Big Joe Launch
September 9, 1959 
Big Joe Launch from Cape Canaveral

October 1959

November 1959

November 4, 1959 
Little Joe 1A launched from Wallops Island

December 1959

December 4 - Sam
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December 4 - Sam
December 4 1959 
LJ-2 launched from Wallops Island carrying Sam
December 15 1959 
The December 1959 edition of SEDR-104 is published containing spacecraft 18, Capsule 19, and Capsule 20 as specification capsules and Capsule 2, Capsule 3, Capsule 4, and Capsule 5 as test capsules
November 15 1959 
Mercury Maintenance Manual SEDR-108 issued

1960

January 1960

Jan 21, 1960? LJ-1B?
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Jan 21, 1960? LJ-1B?
January 21, 1960 
LJ-1B launched from Wallops Island carrying Miss Sam

February 1960

March 1960

April 1960

12 April 1960 
First production model of McDonnell-built Mercury capsule was delivered to NASA

May 1960

May 9 1960 
First production model of Project Mercury spacecraft was successfully launched from NASA Wallops Station to test escape, landing, and recovery systems. Known as the "beach abort" test, the Mercury capsule reached 775 m before parachute landing and pickup by Marine helicopter returned it to Wallops' hangar 17 minutes after launch.
May 14 1960 
The first production Mercury spacecraft, used in the beach-abort test, was returned to the McDonnell plant for an integrity test.
May 23 1960 
Capsule 4 after being instrumented and prepared by the Space Task Group and the Langley Research Center for flight tests, was delivered to Cape Canaveral for the first Mercury-Atlas mission (MA-1).

June 1960

June 16, 1960 Capsule 4 MA-1
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June 16, 1960 Capsule 4 MA-1
June 30 1960 
Capsule 2 delivered to the Marshall Space Flight Center, Huntsville, Alabama, for compatibility tests with the Redstone launch vehicle.


July 1960

23 July 1960 
Capsule 2 delivered to Cape Canaveral for the Mercury-Redstone 1 (MR-1) mission.
29 July 1960 
Capsule 3 delivered to Langley Field for a noise and vibration test.
29 July 1960 
Mercury-Atlas 1 (MA-1) launched. The booster exploded and the spacecraft was destroyed upon impact off-shore.

August 1960

August 5, 1960 
Mercury Manned Orbital Capsule Detailed Specification revised
August 15, 1960 
SEDR-109-7 The Flight Operations Manual for Capsule 7 was issued.
August 16 1960 
At the design engineering inspection of Capsule 7, a number of requests for changes in the control panel area were made by the astronauts to facilitate pilot operation. Later, meeting procedures for design engineering inspections were standardized and conducted by a permanent team at appropriate intervals.
August25 1960 
Mercury Manned Orbital Capsule Detailed Specification revised

September 1960

September 20, 1960 Capsule 2 in ASCS Room
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September 20, 1960 Capsule 2 in ASCS Room
September 23, 1960 Capsule 2 Heatshield and Retro Pkg
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September 23, 1960 Capsule 2 Heatshield and Retro Pkg
3 September 1960 
Aircraft telemetry requirements were deleted from the MA-3 and MA-4 missions, as the spacecraft had been modified to provide telemetry transmissions from the point of main parachute deployment to landing.
29 July 1960 
Capsule 3 delivered to Langley Field for a noise and vibration test.
30 September 1960 
Capsule 5 delivered to the Marshall Space Flight Center for booster compatibility checks


October 1960

October 11 1960 
Capsule 5 shipped to Cape Canaveral

November 1960

Movember 3, 1960 MR-1 Tower Mating
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Movember 3, 1960 MR-1 Tower Mating
November 8, 1960 Escape Tower testing
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November 8, 1960 Escape Tower testing
November 8, 1960 
LJ-5 launched from Wallops Island.
November 13, 1960 
System checkout tests were completed on Capsule 7. In the opinion of McDonnell, the results demonstrated that this spacecraft was adequate for a manned mission.
November 18, 1960 
Capsule 8 Delivered to Cape Canaveral
November 21, 1960 
MR-1 launched from Cape Canaveral


December 1960

December 9 1960 
Capsule 7 delivered to Cape Canaveral.
December 19 1960 
MR-1A launched from Cape Canaveral.

1961

January 1961

January 20, 1961 
Capsule 14 delivered to Wallops Island
January 31, 1961 
MR-2 launched from Cape Canaveral carrying Ham

February 1961

Feb 1, 1961 Capsule 5 in Hangar S
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Feb 1, 1961 Capsule 5 in Hangar S
February 1 1961 
The February 1961 edition of SEDR-104 is published presumably containing Capsule 2, Capsule 3,Capsule 4,Capsule 5, Capsule 6, Capsule 7, Capsule 11. and Capsule 14
Alan Shepard wearing personal parachute
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Alan Shepard wearing personal parachute
February 1 1961 
Instruction was provided to the astronauts to develop techniques and procedures for using the personal parachute as an additional safety feature in the Mercury program. This parachute was only used during the MR-3 mission
w:February 6 1961 
Mercury Capsule 2 configuration specification report 6603-2 revised.
February 17 1961 
The Space Task Group requested that McDonnell design and install a manual bilge pump in Capsule 7 to allow the removal of any seawater resulting from leakage after spacecraft impact.
February 21 1961 
MA-2 launched from Cape Canaveral.
February 24 1961 
Capsule 9 delivered to Cape Canaveral


March 1961

March 2, 1961 
MA-2 flight showed low spacecraft afterbody temperatures.
March 8, 1961 
Capsule 10 delivered to the McDonnell altitude test facility
March 6, 1961 
The third in the series of development engineering inspections on Mercury spacecraft was held. At this time, Capsule 12 and Capsule 15 were inspected, and some 50 requests for alterations were made.
March 7, 1961 
Capsule 11 delivered to Cape Canaveral
March 11, 1961 LJ-5A preparedness chart
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March 11, 1961 LJ-5A preparedness chart
March 17, 1961 Mating dummy capsule for MR-BD
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March 17, 1961 Mating dummy capsule for MR-BD
March 11 1961 
LJ-5A mission preparedness chart
March 16, 1961 
Capsule 10 withdrawn from the flight program and allocated to a ground test simulating orbital flight environmental conditions at the McDonnell plant site.
March 18, 1961 
LJ-5A launched from Wallops Island.

The capsule failed to separate from the Little Joe launch vehicle.
After the failure of this launch Capsule 14 was re-fitted and redesignated as Capsule 14A

March 24, 1961 
MR-BD launched from Cape Canaveral to man-rate the Redstone.


April 1961

April 29, 1961 - Shepard seated in Capsule
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April 29, 1961 - Shepard seated in Capsule
April 4, 1961 
Capsule 14, now re-designated as Capsule 14A, re-delivered to Wallops Island
April 25 1961 
MA-3 launched

The booster was destroyed by the range safety officer. The capsule was returned to McDonnell for refitting and redesignated as Capsule 8A.

April 28 1961 
LJ-5B launched from Wallops Island

May 1961

May 26-June 3, 1961 Freedom 7 at Paris Airshow
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May 26-June 3, 1961 Freedom 7 at Paris Airshow
May 26-June 3, 1961 Freedom 7 at Paris Airshow
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May 26-June 3, 1961 Freedom 7 at Paris Airshow
Early May 1961 
Initial discussion of need for dynamic testing of the Mercury network leading to Mercury Scout
5 May 1961 
MR-3 Launched.
11 May 1961 
Capsule 8 now redesigated as Capsule 8A delivered to Cape Canaveral.
Wikipedia:11 May 1961 
US Air Force reports availability of a Scout missile for the Mercury Scout test.
Wikipedia:15 May 1961
Discussion held of the plans for the Mercury Scout test in preparation for selling it to Abe Silverstein.
Wikipedia:16 May 1961
Abe Silverstein gives tentative NASA HQ approval for Mercury Scout.
23 May 1961 
The fourth development engineering inspection on Mercury spacecraft was held at McDonnell. Inspection activities were primarily centered on Capsule 18, and some 45 requests for alterations were initiated.
26 May 1961
NASA General Manager Robert Seamans gives final NASA HQ approval for Mercury Scout, NASA will fund the payload, while the Air Force would absorb the cost of the Scout.
26 May 1961 
Freedom 7 displayed at Paris Air Show.


June 1961

13 June 1961 
Freedom 7 exhibited in Rome
24 June 1961 
Modifications were made to Capsule 11, the spacecraft designated for the second manned suborbital Mercury flight. An observation window replaced two view ports and an improved manual control system was installed.
28 June 1961 
Capsule 5 in seaworthiness test conducted 65 miles east of Wallops Island.

July 1961

July 21, 1961 Grissom inserted into Liberty Bell 7
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July 21, 1961 Grissom inserted into Liberty Bell 7
21 July 1961 
MR-4 launched

Capsule 11 sank when the side hatch unexpectedly opened during helicopter recovery operations.

August 1961

1 August 1961 
The August 1961 edition of SEDR-104 is published presumably covering Capsule 2, Capsule 3, Capsule 4, Capsule 5, Capsule 6, Capsule 7, Capsule 11, and Capsule 14.
13 August 1961 
Capsule 15 delivered to Cape Canaveral.
It was returned to McDonnell to be reconfigured to the orbital-manned 1-day mission and tentatively assigned for Mercury-Atlas 10 (MA-10). Redesign was completed, and the spacecraft, then designated Capsule 15A (later redesignated Capsule 15B), was delivered to Cape Canaveral on November 16, 1962.


15 August 1961 
Originally planned launch of Mercury Scout test of the Mercury Tracking Network.
27 August 1961 
Capsule 13 Shipped to Cape Canaveral
30 August 1961 
An investigation was conducted as a result of the premature activation of the Mercury-Redstone 4 (MR-4) explosive egress hatch. Tests were initiated in an environment more severe than had been conducted in prelaunch activities and tests, but no premature firings occurred. As a backup, McDonnell was asked to design a mechanical-type hatch. The model weighed some 60 pounds more than the explosive type, so other methods had to be sought to prevent any recurrence of the incident. A procedure was initiated which stipulated that the firing plunger safety pin would be left in place until the helicopter hook was attached to the spacecraft and tension was applied to the recovery cable.

September 1961

September 13, 1961 
MA-4 launched from Cape Canaveral.
September 22 1961 
The Space Task Group announced that a 30-inch diameter balloon would be installed in the Mercury spacecraft to allow for ship recovery should the helicopter be forced to drop the spacecraft, as happened during the Mercury-Redstone 4 (MR-4) recovery operations.

October 1961

October 30 Top of recovery compartment taken in Hangar S
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October 30 Top of recovery compartment taken in Hangar S
1 October 1961 
Capsule 12 delivered to Cape Canaveral

It was a backup for the MA-8 mission (six-orbit flight), but immediate consideration was given for its modification to the Mercury extended range or 1-day mission. The capsule was returned to McDonnell, reconfigured and stored.

23 October 1961 
Freedom 7 presented to the Smithsonian
25 October 1961 
NASA Headquarters officially approved the Mercury extended range or 1-day mission program


November 1961

November 1 1961 
The November 1961 edition of SEDR-104 is issued covering Capsule 18, and Capsule 19 as specification capsules, Capsule 8, Capsule 9, Capsule 10, Capsule 13, Capsule 16 as test capsules and stating that Capsule 12, Capsule 15, Capsule 17, and Capsule 20 had been assigned to be configured for an 18 orbit mission.
November 15 1961 
Capsule 18 delivered to Cape Canaveral.
November 29 1961 
MA-5 Launched from Cape Canaveral carrying Enos

December 1961

December 11 and December 13, 1961 
John Glenn and Scott Carpenter, along with Donald Slayton and Walter Schirra, already picked for MA-7, participated in a two-day recovery exercise on the Back River near Langley Air Force

1962

January 1962

10 January 1963 
Capsule 9 was cycled through Project Orbit Mission Runs 108, 108A, and 108B in the test facilities of the McDonnell Aircraft Corporation.
16 January 1962 
Capsule 16 delivered to Cape Canaveral
18 January 1962 
The Mercury Capsule No. 16 Configuration Specification is published by McDonnell

February 1962

1 February 1962 
The February 1962 edition of SEDR-104 is published covering Capsule 19 as a specification capsule, Capsule 8, Capsule 9, Capsule 13, Capsule 16, Capsule 18 as test capsules
20 February 1962 
MA-6 Launched

March 1962

4 March 1962 Scott Carpenter and Walter Schirra, designated (but not publicly) as pilot and backup pilot, respectively, for the Mercury-Atlas 7 (MA-7) manned orbital mission, underwent water-egress exercises. Several side-hatch egresses were made in conjunction with helicopter pickups.

20 March 1962 
Capsule 19 delivered to Cape Canaveral

April 1962

April 25, 1962 DUMMY heat shield and retro package for MA-7
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April 25, 1962 DUMMY heat shield and retro package for MA-7
April 26, 1962 Capsule 18 in Weight and Balance
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April 26, 1962 Capsule 18 in Weight and Balance
April 19 1962 
Capsule 7 goes on world tour


May 1962

May 13, 1962 - MA-7 Recovery compartment
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May 13, 1962 - MA-7 Recovery compartment
May 1 1962 
The May 1962 edition of SEDR-104 is published which covers Capsule 12, Capsule 15, Capsule 17, and Capsule 20.
May 1 1962 
The decision was made between April 29 and May 5, 1962, that leg supports would be removed from the astronaut's couch. It had been determined that the heel and toe supports could be used as the sole supports for the lower leg.
May 24 1962 
MA-7 launched.
May 28 1962 
For possible application purposes, and upon request, the Manned Spacecraft Center shipped Mercury-type survival kits to the Air Force for its X-20 Dyna Soar development program and to the Navy.
May 28 1962 
Flight and ground tests disclosed that retrorocket heater blankets were unnecessary to the spacecraft, and this item was removed.


June 1962

26 June 1962 
Project Reef, an airdrop program to evaluate the Mercury 63-foot ringsail main parachute's capability to support the higher spacecraft weight for the extended range or 1-day mission was completed. Tests indicated that the parachute qualified to support the mission.
28 June 1962 
The Manned Spacecraft Center requested that the Langley Research Center participate in acoustic tests of ablation materials on Mercury flight tests. Langley was to prepare several material specimens which would be tested for possible application in providing lightweight afterbody heat protection for Apollo class vehicles. Langley reported the results of its test preparation activities on September 21, 1962.
29 June 1962 
Engineering was completed for the spacecraft reaction control system reserve fuel tank and related hardware in support of the Mercury extended range or 1-day mission.

July 1962

13 July 1962 
Tests were conducted with a subject wearing a Mercury pressure suit in a modified Mercury spacecraft couch equipped with a B-70 (Valkyrie) harness. When this harness appeared to offer advantages over the existing Mercury harness, plans were made for further evaluation in spacecraft tests.

August 1962

August 31, 1962 Artists concept of Mercury Capsule
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August 31, 1962 Artists concept of Mercury Capsule
August 6 1962 
Friendship 7 spacecraft placed on display at the Century 21 Exposition in Seattle, Washington
August 8 1962 
Capsule 9 (redesignated Capsule 9A) was phased into the Project Orbit program in preparation for the Mercury extended range or 1-day mission.
August 11 1962 
Mercury spacecraft reaction control system test was completed. Data compiled from this test was used to evaluate the thermal and thruster configuration of the Mercury extended range or 1-day mission spacecraft.
August 19 1962 
Negotiations were completed with McDonnell for spacecraft configuration changes to support the Mercury 1-day manned orbital mission. The design engineering inspection, when the necessary modifications were listed, was held on June 7, 1962.


September 1962

September 19, Wally Schirra in pre-flight checkout
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September 19, Wally Schirra in pre-flight checkout
September 26, MA-8 Re-mating
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September 26, MA-8 Re-mating
September 28, MA-8 Ditty bag contents
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September 28, MA-8 Ditty bag contents
18 September 1962 
The NASA spacecraft test conductor and the Convair test conductor notified the interface committee chairman of the readiness-for-mate of the adapter-interface area of the Mercury-Atlas 8 MA-8.
22 September 1962 
As an experiment, Wally Schirra planned to carry a special 2.5-pound hand camera aboard the Mercury-Atlas 8 MA-8 Capsule 16. During the flight, the astronaut would attempt to arrive at techniques that could be applied to an advanced Nimbus weather satellite.


October 1962

3 October 1962 
MA-8 launched.
5 October 1962 
Capsule 16 was returned to Hanger S at Cape Canaveral for postflight work and inspection. It was planned to retain the Sigma 7 capsule at Cape Canaveral for permanent display.
5 October 1962 
Capsule 20 delivered to Cape Canaveral.
19 October 1962 
All spacecraft system tests reported complete for Capsule 20

November 1962

16 November 1962 
Capsule 15A delivered to Cape Canaveral
26 November 1962 
Mercury Capsule No. 15A Configuration Specification issued

December 1962

1 December 1962 
The December 1962 edition of SEDR-104 is published which covers Capsule 20.

1963

January 1963

10 January 1963 
Capsule 9 was cycled through Project Orbit Mission Runs 108, 108A, and 108B in the test facilities of the McDonnell Aircraft Corporation.
11 January 1963 
The Project Engineering Field Office (located at Cape Canaveral) of the Mercury Project Office reported on the number of changes made to Capsule 20 for MA-9 as of that date after its receipt at Cape Canaveral from McDonnell in St. Louis. There were 17 specific changes, which follow: one to the reaction control system, one to the environmental control system, seven to the electrical and sequential systems, and eight to the console panels.
14 January 1963 
In the event MA-10 were flown, Capsule 15 now once again re-designated as Capsule 15B would be the prime spacecraft. Modifications were started immediately with respect to the hand controller rigging procedures, pitch and yaw control valves, and other technical changes.
22 January 1963 
McDonnell Aircraft Corporation reported to the Manned Spacecraft Center on a study conducted to ascertain temperature effects on the spacecraft as a result of white paint patch experiments on Capsule 16 during MA-8

February 1963

February 2, 1963
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February 2, 1963
February 5 1963 
Personnel of the Manned Spacecraft Center visited the McDonnell plant in St. Louis to conduct a spacecraft status review. Units being inspected were Capsule 15B and Capsule 20. In addition, the status of the Gemini Simulator Instructor Console was assessed. With regard to the spacecraft inspection portion, a number of modifications had been made that would affect the simulator trainers. On spacecraft 15B, 15 modifications were made to the control panel and interior, including the relocation of the water separator lights, the addition of water spray and radiation experiment switches and a retropack battery switch. The exterior of the spacecraft underwent changes as well, involving such modifications as electrical connections and redesign of the fuel system for the longer mission. The reviewers found that spacecraft 20 conformed closely to the existing simulator configuration, so that modifications to the simulator were unnecessary.
February 7 1963 
At a Development Engineering Inspection for the Capsule 15B mockup, designated for the MA-10 mission, some 42 requests for alterations were listed.
February 20 1963 
Friendship 7 spacecraft presented to the Smithsonian Institution.
February 23 1963 
Manned Spacecraft Center checkout and special hardware installation at Cape Canaveral on Capsule 20 were scheduled for completion as of this date. However, work tasks were extended for a 2-week period because of the deletion of certain experimental hardware - zero g experiment and new astronaut couch. In addition, some difficulties were experienced while testing the space reaction control system and environmental control system.

March 1963

11 March 1963 
Based on a request from the Manned Spacecraft Center, McDonnell submitted a review of clearances between the Mercury Capsule 15B retropack and the launch vehicle adapter during separation maneuvers. This review was prompted by the fact that additional batteries and a water tank had been installed on the sides of the retropack. According to the McDonnell study the clearance safety margin was quite adequate.
19 March 1963 
The Manned Spacecraft Center received a slow-scan television camera system, fabricated by Lear Siegler, Incorporated, for integration with Capsule 20 for the MA-9 mission.

April 1963

April 18, S/C 20 in Weight and Balance
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April 18, S/C 20 in Weight and Balance
April 20 1963 
The final water condensate tank was installed in Capsule 20 for the MA-9 mission. In all, the system consisted of a 4-pound, built-in tank, a 3.6 pound auxiliary tank located under the couch head, and six 1-pound auxiliary plastic containers. The total capacity for condensate water storage was 13.6 pounds. In operation, the astronaut hand-pumped the fluid to the 3.6 pound tank to avoid spilling moisture inside the cabin from the built-in tank. Then the 1-pound containers were available.
April 22 1963 
Capsule 20 was moved from Hanger S at Cape Canaveral to Complex 14 and mated to Atlas launch vehicle 130-D in preparation for the Mercury-Atlas 9 MA-9 mission. The first simulated flight test was begun immediately.


May 1963

May 9, Cooper in pre-flight check
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May 9, Cooper in pre-flight check
15 May 1963 
MA-9 launched.


June 1963

6 June 1963 
Officials of the Manned Spacecraft Center made a presentation to NASA Administrator James E. Webb, outlining the benefits of continuing Project Mercury at least through the Mercury-Atlas 10 MA-10 mission. They thought that the spacecraft was capable of much longer missions and that much could be learned about the effects of space environment from a mission lasting several days. This information could be applied to the forthcoming Projects Gemini and Apollo and could be gained rather cheaply since the MA-10 launch vehicle and spacecraft were available and nearing a flight readiness status.
8 June 1963 
In preparation for the Mercury-Atlas 10 MA-10 mission, should the flight be approved by NASA Headquarters, several environmental control system changes were made in Capsule 15B. Particularly involved were improvements in the hardware and flexibility of the urine and condensate systems. With regard to the condensate portion, Gordon Cooper, in his press conference, indicated that the system was not easy to operate during the flight of Faith 7 MA-9.
12 June 1963 
Testifying before the Senate Space Committee, James E. Webb, the NASA Administrator, said: 'There will be no further Mercury shots . . .' He felt that the manned space flight energies and personnel should focus on the Gemini and Apollo programs. Thus, after a period of 4 years, 8 months, and 1 week, Project Mercury, America's first manned space flight program, came to a close.
13 June 1963 
McDonnell's Project Mercury contract was terminated. McDonnell had already essentially concluded its Mercury activities and Capsule 15B had been delivered to Cape Canaveral. A termination meeting held at the Manned Spacecraft Center on June 14 settled the disposition of Mercury property and personnel. McDonnell was to screen all Mercury property for possible use in the Gemini program; any property McDonnell claimed would be transferred to Gemini by authority of the contracting officer at St Louis or the Cape. McDonnell was directed to furnish Gemini Project Office with a list of key Mercury personnel who might be reassigned to Gemini.

October 1963

These images were found on the JSC web site and are here because that site gives an October 1963 date for them. This may indicate that a report with this date included these images. The date is suspiciouse because the Mercury program had already ended.

October 21, 1963?
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October 21, 1963?
October 22, 1963?
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October 22, 1963?
October 22, 1963?
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October 22, 1963?
October 22, 1963?
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October 22, 1963?


1999

July 1999

Spacecraft 11 finally comes home
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Spacecraft 11 finally comes home
July 20, 1999 
Capsule 11 Recovered from ocean bottom
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