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KENNEDY SPACE CENTER, FLA. - Technicians attach a crane to the Pump Flow Control Subsystem (PFCS) in the Space Station Processing Facility. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital Replacement Units on the Integrated Equipment Assembly that make up the S6 Photo-Voltaic Power Module on the International Space Station (ISS). The fourth starboard truss segment, the S6 Truss measures 112 feet long by 39 feet wide. Its solar arrays are mounted on a “blanket” that can be folded like an accordion for delivery to the ISS. Once in orbit, astronauts will deploy the blankets to their full size. When completed, the Station's electrical power system (EPS) will use eight photovoltaic solar arrays to convert sunlight to electricity. Delivery of the S6 Truss, the last power module truss segment, is targeted for mission STS-119. KSC-04pd1477
KENNEDY SPACE CENTER, FLA. -- Inside the payload bay of Space Shuttle orbiter Endeavour, workers and STS-88 crew members on a movable work platform or bucket move closer to the rear of the orbiter's crew compartment. While Endeavour is being prepared for flight inside Orbiter Processing Facility Bay 1, the STS-88 crew members are participating in a Crew Equipment Interface Test (CEIT) to familiarize themselves with the orbiter's midbody and crew compartments. A KSC worker (left) maneuvers the platform to give Mission Specialists Jerry L. Ross and James H. Newman (right) a closer look. Looking on is Wayne Wedlake of United Space Alliance at Johnson Space Center. Targeted for liftoff on Dec. 3, 1998, STS-88 will be the first Space Shuttle launch for assembly of the International Space Station (ISS). The primary payload is the Unity connecting module which will be mated to the Russian-built Zarya control module, expected to be already on orbit after a November launch from Russia. After the mating, Ross and Newman are scheduled to perform three spacewalks to connect power, data and utility lines and install exterior equipment. The first major U.S.-built component of ISS, Unity will serve as a connecting passageway to living and working areas of the space station. Unity has two attached pressurized mating adapters (PMAs) and one stowage rack installed inside. PMA-1 provides the permanent connection point between Unity and Zarya; PMA-2 will serve as a Space Shuttle docking port. Zarya is a self-supporting active vehicle, providing propulsive control capability and power during the early assembly stages. It also has fuel storage capability KSC-98pc1216
KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility at NASA's Kennedy Space Center, STS-115 crew members inspect equipment in Atlantis's payload bay. From left are Mission Specialists Joseph Tanner and Heidemarie Stefanyshyn-Piper. The crew is at KSC for Crew Equipment Interface Test activities, which involves equipment familiarization, a routine part of astronaut training and launch preparations. The STS-115 mission will deliver the second port truss segment, the P3/P4 truss, to the International Space Station. The crew will attach the P3 to the first port truss segment, the P1 truss, as well as deploy solar array set 2A and 4A. Launch on Space Shuttle Atlantis is scheduled for late August. Photo credit: NASA/Kim Shiflett KSC-06pd1206
KENNEDY SPACE CENTER, Fla. -- From a vantage point below it, members of the STS-110 crew check out Integrated Truss Structure (ITS) S0, which is in the Operations and Checkout Building. From left are Mission Specialists Rex J. Walheim, Jerry L. Ross and Lee M. Morin. They and other crew members are taking part in a Crew Equipment Interface Test at KSC. Not shown are Commander Michael J. Bloomfield, Pilot Stephen N. Frick, and Mission Specialists Steven L. Smith and Ellen Ochoa. The ITS S0 is part of the payload on the mission. It is the center segment they will be installing on the International Space Station, part of the 300-foot (91-meter) truss attached to the U.S. Lab. By assembly completion, four more truss segments will attach to either side of the S0 truss. STS-110 is currently scheduled to launch in February 2002 KSC-01pp1567
Diagnostic equipment is strapped down in a Rapid Assistance
HIGH BAY AREA, NASA Technology Images
US COAST GUARD AMT Competition U.S. Coast Guard photograph
TEST RIGS, NASA Technology Images
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Резюме
(8 апреля 1986 года) 28 января 1986 года космический корабль "Челленджер" и его экипаж из семи человек погибли, когда разрыв О-образного кольца в правой части разгонного блока "Бриз-М" вызвал взрыв вскоре после запуска. После аварии поисково-спасательные команды в течение нескольких месяцев работали над тем, чтобы доставить обломки из Шэньчжэня в места затопления в Космическом центре Кеннеди и на станции ВВС на мысе Канаверал, где восстановительные бригады отделили фрагменты орбитального аппарата от фрагментов внешнего бака и разгонного блока "Бриз-М". Квадраты на полу превратили зоны подтопления в сетку, в которой бригады по реконструкции могли собрать мусор, как лужу, со многими отсутствующими сегментами. Здесь собран "Орбитальный аппарат".
Коллекция фотографий НАСА
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Тэги
стс 51 л претендент обломки
орбитальный аппарат
авария космического челнока
бригады реконструкции
водохранилища
обломки
правый твердотопливный ракетный ускоритель
обломки шаттла
космический челнок претендент
твердотопливные ракетные ускорители
мыс Канаверал военно-воздушная база
шт
Космический центр Кеннеди
команды восстановления
челнок
внешний бак
НАСА
Дата
1986
в коллекциях
Месторасположение
Источник
NASA
Ссылка
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