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john f. kennedy space center brevard county, florida - Environmental ...

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The third floor contains the four firing rooms, referred to as Control Rooms 1 through 4, from<br />

west to east. Each measures 175 ft in length and 85 ft in width. Firing Rooms 1 and 3 are<br />

configured for full control of launch and Orbiter operations. At the <strong>center</strong> front of the rooms is a<br />

series of three stepped platforms, with a triangular enclosed room in each corner. The west<br />

corner room serves as the Operations Support Room, while the east corner room serves as the<br />

Operations Management Room. The highest of the three central platforms contains consoles for<br />

the Public Affairs Officer, the weather monitor, and the Launch Director. The middle platform<br />

includes the stations for the Orbiter Test Director, the NASA Test Director, and the Support Test<br />

Manager. The lowest platform has stations for the Safety Console Coordinator, the Payload Test<br />

Conductor and the Booster Test Conductor.<br />

The remainder of the Control Room sits on a level surface and includes three single groups of<br />

consoles (C-1, HSP-2, and C-2) at the front, and six paired consoles to the rear (C-3 and C-4; C-5<br />

and C-6; C-7 and C-8; C-9 and C-10; C-11 and C-12; Backup and Integration). The C-1 console<br />

controls operations; HSP-2 is a spare console, used if another should become unavailable; and C-<br />

2 monitors the navigation aids, communications equipment, the mechanical systems on the<br />

orbiter, and the payload electrical systems. The C-3 and C-4 combination monitors the orbiter’s<br />

cryogenics and main propulsions systems, while the C-5 and C-6 consoles control the Range<br />

Safety System, the <strong>Environmental</strong> Control and Life Support System, the <strong>Environmental</strong> Control<br />

Systems, and the Power Reactant and Storage Distribution System. The C-7 and C-8 consoles are<br />

responsible for two swingarms on the launch pad, the hypergolic fuels, monitoring the hypergolic<br />

pressure, and controlling the auxiliary power units and the hydraulic power units. The<br />

combination C-9 and C-10 consoles monitor hazardous gas levels, as well as the orbiter’s<br />

instrumentation and electrical power systems; the C-11 and C-12 consoles monitor the orbiter’s<br />

avionics systems. The Backup and Integration consoles provide additional spares. At the very<br />

back of the Control Room, in a partitioned <strong>space</strong>, is the Master Console, which controls the<br />

configurations for all others in the Control Room.<br />

The remaining two firing rooms, Firing Room 2 and Firing Room 4, are not fully equipped to<br />

serve as launch control rooms. Firing Room 2 is generally used for software development and<br />

testing, and Firing Room 4 is partially equipped as a launch control room, but is primarily used as<br />

an engineering analysis and support area for launch and checkout operations. All four firing<br />

rooms have a suspended floor that allows cables to be run throughout the floor and the equipment<br />

to be cooled. In addition to the firing rooms, the third floor contains two visitor’s galleries, each<br />

of which measures approximately 25 ft by 16 ft. The first of these sits between Control Rooms 1<br />

and 2; the second between Control Rooms 3 and 4. The fourth floor of the LCC contains office<br />

areas, conference rooms, and mechanical equipment.<br />

The resource boundary extends from the outer footprint of the Launch Control Center,<br />

approximately 10 feet, which includes the facility and all necessary components historically<br />

required for its functions.<br />

SIGNIFICANCE: The LCC was listed in the NRHP on January 21, 2000. Originally nominated<br />

in the context of the Apollo Program, ca. 1961 through 1975, the LCC has since gained<br />

importance in the context of the Space Shuttle program, ca. 1969 to 2010. It is considered<br />

significant at the national level under NRHP Criterion A in the areas of Space Exploration and<br />

Communications, and under NRHP Criterion C in the area of Architecture. Because the LCC has<br />

achieved significance within the past 50 years, Criteria Consideration G applies. The period of<br />

significance for the LCC is from 1980, when vehicle preparations for the first Space Shuttle<br />

launch began, through 2010, the designated end of the Space Shuttle Program. The Space Shuttle

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