The monument was designed with advice from the staff at the Smithsonian National Air and Space Museum to ensure that it was historically accurate.
23 at the First Americans Museum in Ross' home state of Oklahoma. 7), ahead of it going on public display on Feb.
Agena rocket skin#
Olay, the skin care company, is unveiling the new statue of Ross on Monday (Feb. Now, a new statue of the trailblazing Native American woman will help steer a new generation toward the stars. Sustainer cutoff timer failed, causing the Atlas to burn to propellant depletion and putting the payload in a higher than planned orbit.- In life, Mary Golda Ross helped develop a rocket stage that served as a rendezvous and docking target for astronauts preparing to go to the moon. Nose cone separated properly, but was lost at sea after recovery crews failed to locate it. Sustainer hydraulic system leak at staging results in loss of hydraulic fluid and engine shutdown. Intermittently shorted diode in guidance system results in premature propulsion system cutoff. Agena separated but was left facing in the wrong direction for orbital insertion. RSO T+35 seconds.Īgena failed to restart due to rate gyro malfunction spacecraft left in LEO. Sustainer engine shut down at liftoff due to improperly installed pressure transducer. Roll control failed T+186 seconds, satellite placed in an incorrect orbit Vehicle fell back onto the pad and exploded.
Improper umbilical eject sequence causes loss of electrical power.
Agena rocket generator#
Sustainer engine lost thrust due to gas generator failure following booster staging. Gyro spin motor set to incorrect speed, causing excessive pitch rate and missile self-destruction at T+101 seconds.Īgena failed to restart due to electrical short spacecraft left in LEO.
Vehicle exploded at liftoff due to combustion instability in the B-1 engine. Capsule successfully recovered.įirst attempted launch of an Atlas E from VAFB. Pitch and roll sequence failed to initiate due to short or open circuit in missile programmer. Wiring error results in loss of helium control bottle gas, no gas left to perform booster jettisonįirst attempted orbital Mercury launch. Propellant utilization malfunction results in premature fuel depletion and sustainer shutdown Vibration and/or flying debris from Able adapter section ruptured Atlas LOX tank T+66 seconds, followed by complete vehicle self-destruction at T+73 seconds.Īerodynamic heating shorted the vernier feedback transducer, resulting in unstable flight trajectoryįirst successful launch of a Mercury-Atlas Missile tumbled following staging, but remained structurally intact until impact with the ocean. Sustainer hydraulic rise-off disconnect failed due to radiated heat, causing loss of hydraulic fluid and sustainer shutdown T+40 seconds. Overpressurization of the LOX tank ruptured the intermediate bulkhead followed by missile self-destruction at T+71 seconds. LOX tank sensing line rise-off disconnect failed due to radiated heat. Improper pad umbilical disconnect caused loss of Agena pressurization gas. Missile tumbled following staging and broke up at T+154 seconds. Missile impacted 1200 miles off target.įirst Atlas E launch. Staging electrical disconnect plug pulled out T+125 seconds, causing premature BECO and failure of booster section to jettison.
Sustainer engine lost thrust due to failure of helium control pressure First attempted launch of a Mercury capsule.Ītlas portion of flight successful, RVX-2A reentry vehicle not recovered Gyro spin motor failure resulted in an unplanned pitch maneuver that exceeded the missile's structural limits and caused vehicle breakup at T+69 seconds.Įxcessive aerodynamic bending of the Mercury adapter interface results in Atlas structural failure T+58 seconds. The missile impacted 40 miles short of its intended target point. Short in relay box caused decrease in propulsion system performance. Pitch gyro motor shorted, causing loss of control. Missile fell back onto the pad and exploded.Ĭombustion instability in B-2 engine. First launch of the Atlas-Agena vehicle.Ĭombustion instability in B-1 engine. Agena RSO charges accidentally fired at staging, leading to vehicle breakup.
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