Mercury-Redstone 1A
Mercury-Redstone 1A was launched on December 19, 1960 from LC-5 at Cape Canaveral, Florida. The mission objectives of this unmanned 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 and a range of. The launch vehicle reached a slightly higher velocity than expected -. 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.
Current location
Mercury spacecraft #2, used in both the Mercury-Redstone 1 and Mercury-Redstone 1A missions, is currently displayed at the NASA Ames Exploration Center, Moffett Federal Airfield, near Mountain View, California.Mercury-Redstone suborbital flight events
T+ Time | Event | Description |
T+00:00:00 | Liftoff | Mercury-Redstone lifts off, onboard clock starts. |
T+00:00:16 | Pitch Program | Redstone pitches over 2 deg/s from 90 deg to 45 deg. |
T+00:00:40 | End Pitch Program | Redstone reaches 45 deg pitch. |
T+00:01:24 | Max Q | Maximum dynamic pressure ~ |
T+00:02:20 | BECO | Redstone engine shutdown - Booster Engine Cutoff. Velocity |
T+00:02:22 | Tower Jettison | Escape Tower Jettison |
T+00:02:24 | Capsule Separation | Posigrade rockets fire for 1 s giving separation. |
T+00:02:35 | Turnaround Maneuver | Capsule system rotates capsule 180 degrees, to heat shield forward attitude. Nose is pitched down 34 degrees to retro fire position. |
T+00:05:00 | Apogee | Apogee of about reached at downrange from launch site. |
T+00:05:15 | Retrofire | Three retrorockets fire for 10 seconds each. They are started at 5 second intervals, firing overlaps. Delta V of is taken off forward velocity. |
T+00:05:45 | Retract Periscope | Periscope is automatically retracted in preparation for reentry. |
T+00:06:15 | Retro Pack Jettison | One minute after retrofire retro pack is jettisoned, leaving heatshield clear. |
T+00:06:20 | Retro Attitude Maneuver | orients capsule in 34 degrees nose down pitch, 0 degrees roll, 0 degrees yaw. |
T+00:07:15 | .05 G Maneuver | detects beginning of reentry and rolls capsule at 10 deg/s to stabilize capsule during reentry. |
T+00:09:38 | Drogue Parachute Deploy | Drogue parachute deployed at slowing descent to and stabilizing capsule. |
T+00:09:45 | Snorkel Deploy | Fresh air snorkel deploys at. switches to emergency oxygen rate to cool cabin. |
T+00:10:15 | Main Parachute Deploy | Main parachute deploys at. Descent rate slows to. |
T+00:10:20 | Landing Bag Deploy | Landing Bag Deploys, dropping heat shield down. |
T+00:10:20 | Fuel Dump | Remaining hydrogen peroxide fuel automatically dumped. |
T+00:15:30 | Splashdown | Capsule lands in water about downrange from launch site. |
T+00:15:30 | Rescue Aids Deploy | Rescue aid package deployed. The package includes green dye marker, recovery radio beacon and whip antenna. |