ВНИМАНИЕ! На форуме начался конкурс - астрофотография месяца ИЮЛЬ!
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Сегодня на космодроме Байконур после заседания Государственной комиссии, которая утвердила состав основного и дублирующего экипажей транспортного пилотируемого корабля «Союз ТМА-22», состоялась традиционная предполетная пресс-конференция космонавтов и астронавтов. Космонавты и астронавты ответили на вопросы журналистов, в том числе о предстоящей работе на орбите и участии в научных экспериментах.
У меня вопрос возник - американец ходит в очках, у него близорукость или дальнозоркость и сколько диоптрий? Разве в астронавты можно попасть имея нарушение зрения. Спасибо.
Basic requirements for a Mission Specialist include the following: 1. Bachelor's degree from an accredited institution in engineering, biological science, physical science, or mathematics. Degree must be followed by at least three years of related, progressively responsible, professional experience. An advanced degree is desirable and may be substituted for part or all of the experience requirement (master's degree = 1 year of experience, doctoral degree = 3 years of experience). Quality of academic preparation is important. 2. Ability to pass a NASA space physical, which is similar to a military or civilian flight physical and includes the following specific standards:Distance visual acuity: 20/200 or better uncorrected, correctable to 20/20, each eye.Blood pressure: 140/90 measured in a sitting position.3. Height between 58.5 and 76 inches.
Начало: 05:14:00 14.11.2011 (Время московское, МСКЛВ). Окончание: 09:14:00 14.11.2011 (Время московское, МСКЛВ). Время запуска: 08:14:05 14.11.2011 (Время московское, МСКЛВ).
T- 34 Hours Booster is prepared for fuel loadingT- 6:00:00 Batteries are installed in boosterT- 5:30:00 State commission gives go to take launch vehicleT- 5:15:00 Crew arrives at site 254T- 5:00:00 Tanking beginsT- 4:20:00 Spacesuit donningT- 4:00:00 Booster is loaded with liquid oxygenT- 3:40:00 Crew meets delegationsT- 3:10:00 Reports to the State commissionT- 3:05:00 Transfer to the launch padT- 3:00:00 Vehicle first and second stage oxidizer fueling completeT- 2:35:00 Crew arrives at launch vehicleT- 2:30:00 Crew ingress through orbital module side hatchT- 2:00:00 Crew in re-entry vehicleT- 1:45:00 Re-entry vehicle hardware testedSuits are ventilatedT- 1:30:00 Launch command monitoring and supply unit preparedOrbital compartment hatch tested for sealingT- 1:00:00 Launch vehicle control system prepared for use; gyro instruments activatedT - :45:00 Launch pad service structure halves are loweredT- :40:00 Re-entry vehicle hardware testing complete; leak checks performed on suitsT- :30:00 Emergency escape system armed; launch command supply unit activatedT- :25:00 Service towers withdrawnT- :15:00 Suit leak tests complete; crew engages personal escape hardware auto modeT- :10:00 Launch gyro instruments uncaged; crew activates on-board recordersT- 7:00 All prelaunch operations are completeT- 6:15 Key to launch command given at the launch siteAutomatic program of final launch operations is activatedT- 6:00 All launch complex and vehicle systems ready for launchT- 5:00 Onboard systems switched to onboard controlGround measurement system activated by RUN 1 commandCommander's controls activatedCrew switches to suit air by closing helmetsLaunch key inserted in launch bunkerT- 3:15 Combustion chambers of side and central engine pods purged with nitrogenT- 2:30 Booster propellant tank pressurization startsOnboard measurement system activated by RUN 2 commandPrelaunch pressurization of all tanks with nitrogen beginsT- 2:15 Oxidizer and fuel drain and safety valves of launch vehicle are closedGround filling of oxidizer and nitrogen to the launch vehicle is terminatedT- 1:00 Vehicle on internal powerAutomatic sequencer onFirst umbilical tower separates from boosterT- :40 Ground power supply umbilical to third stage is disconnectedT- :20 Launch command given at the launch positionCentral and side pod engines are turned onT- :15 Second umbilical tower separates from boosterT- :10 Engine turbopumps at flight speedT- :05 First stage engines at maximum thrustT- :00 Fueling tower separates Lift off
Разводят колонны:
Какова вероятность, что старт будет успешный?