Mercury-Redstone 1A

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Mercury-Redstone 1A
Mercury Spacecraft at NASA Ames.JPG
Mercury spacecraft #2, used on both the MR-1 and MR-1A flights, on display at NASA Ames Exploration Center.
Mission typeTest flight
Operator NASA
COSPAR ID OOjs UI icon edit-ltr-progressive.svg
Mission duration15 minutes, 45 seconds
Distance travelled378.2 kilometers (235.0 mi)
Apogee210.3 kilometers (130.7 mi)
Spacecraft properties
Spacecraft Mercury No.2
Manufacturer McDonnell Aircraft
Launch mass1,230 kilograms (2,720 lb) [1] [note 1]
Start of mission
Launch dateDecember 19, 1960, 16:15 (1960-12-19UTC16:15Z) UTC
Rocket Redstone MRLV MR-3
Launch site Cape Canaveral LC-5
End of mission
Recovered by USS Valley Forge
Landing dateDecember 19, 1960, 16:30 (1960-12-19UTC16:31Z) UTC
 

Mercury-Redstone 1A (MR-1A) was launched on December 19, 1960 from LC-5 at Cape Canaveral, Florida. The mission objectives of this uncrewed suborbital flight were to qualify the spacecraft for space flight and qualify the system for an upcoming primate suborbital flight. The spacecraft tested its instrumentation, posigrade rockets, retrorockets and recovery system. The mission was completely successful. The Mercury capsule reached an altitude of 130 miles (210 km) and a range of 235 miles (378 km). The launch vehicle reached a slightly higher velocity than expected - 4,909 miles per hour (7,900 km/h). The Mercury spacecraft was recovered from the Atlantic Ocean by recovery helicopters about 15 minutes after landing. Serial numbers: Mercury Spacecraft #2 was reflown on MR-1A, together with the escape tower from Capsule #8 and the antenna fairing from Capsule #10. Redstone MRLV-3 was used. The flight time was 15 minutes and 45 seconds.

Contents

Mercury-Redstone suborbital flight events

MR-1A Launch MR-1A liftoff.jpg
MR-1A Launch
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 lb/sq ft (27,500 Pa)
T+00:02:20BECORedstone engine shutdown - Booster Engine Cutoff. Velocity 5,200 mph (8,400 km/h)
T+00:02:22Tower JettisonEscape Tower Jettison
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 retrorockets fire for 10 seconds each. They are started at 5 second intervals, firing overlaps. Delta V of 550 ft/s (170 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 heatshield clear.
T+00:06:20Retro Attitude Maneuver(ASCS) orients capsule in 34 degrees nose down pitch, 0 degrees roll, 0 degrees yaw.
T+00:07:15.05 G 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 (6,700 m) slowing descent to 365 ft/s (111 m/s) and stabilizing capsule.
T+00:09:45Snorkel DeployFresh air snorkel deploys at 20,000 ft (6,100 m). (ECS) switches to emergency oxygen rate to cool cabin.
T+00:10:15Main Parachute DeployMain parachute deploys at 10,000 ft (3,000 m). Descent rate slows to 30 ft/s (9.1 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 miles (480 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.

Current location

Mercury spacecraft #2, used in both the Mercury-Redstone 1 and Mercury-Redstone 1A missions, was displayed at the NASA Ames Exploration Center, Moffett Federal Airfield, near Mountain View, California [2] until 2022 when it was relocated to the Cradle of Aviation Museum in Garden City, NY. [3]

Notes

  1. This is the mass of the spacecraft after separation from the booster, including all spacecraft consumables. It excludes the escape tower, which was jettisoned before spacecraft separation, and the spacecraft-booster adapter, which remained attached to the booster. Note that Mercury spacecraft #2 lacked some of the equipment present in the spacecraft used on the crewed Mercury flights.

See also

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References

PD-icon.svg This article incorporates  public domain material from websites or documents ofthe National Aeronautics and Space Administration .

  1. Korando, R. D. (February 6, 1961). Mercury Capsule No. 2 Configuration Specification (Mercury-Redstone No. 1) (PDF). St. Louis, Missouri: McDonnell Aircraft Corporation. pp. 7–9. Report number NASA-CR-137390.
  2. "NASA Ames Exploration Center". NASA Ames Research Center . Retrieved 2009-05-14.
  3. "First NASA capsule to fly into space lands at Long Island museum". CollectSpace. Retrieved 26 July 2022.