NASA Home Page NASA Home PageJohn F. Kennedy Space Center - NASA Facts On Line

KSC Home Page Site Search FAQ's Site Survey Customer Forum NASA Centers Privacy Statement Headlines

Countdown! NASA Launch Vehicles and Facilities
PMS 018-B 
October 1991
Section 4

 

Sound Suppression Water System

Previous Section

Next Section

Table  of Contents KSC Fact Sheets Next Page Top

A Sound Suppression Water System has been installed on the pads to protect the orbiter and its payloads from damage by acoustical energy and rocket exhaust reflected from the flame trench and Mobile Launcher Platform during launch. The Shuttle orbiter, with its payloads in the cargo hold, is much closer to the surface of the Mobile Launcher Platform than the Apollo spacecraft was at the top of a Saturn V or Saturn 1B vehicle.

The Sound Suppression System includes an elevated water tank with a capacity of 300,000 gallons (1,135,620 liters). The tank is 290 feet (88 meters) high and is located adjacent to each pad. The water releases just prior to the ignition of the Shuttle engines, and flows through 7-foot-diameter (2.1-meter) pipes for about 20 seconds. Water pours from 16 nozzles atop the flame deflectors and from outlets in the main engines exhaust hole in the Mobile Launcher Platform, starting at T minus 6.6 seconds. By the time the solid rocket boosters ignite, a torrent of water will be flowing onto the Mobile Launcher Platform from six large quench nozzles, or "rainbirds," mounted on its surface.

The rainbirds are 12 feet (3.7 meters) high. The two in the center are 42 inches (107 centimeters) in diameter; the other four have a 30-inch (76-centimeter) diameter.

The peak rate of flow from all sources is 900,000 gallons (3,406,860 liters) of water per minute at 9 seconds after liftoff.

Acoustical levels reach their peak when the Space Shuttle is about 300 feet (91 meters) above the Platform, and cease to be a problem at an altitude of about 1,000 feet (305 meters).

Solid Rocket Booster Overpressure Suppression System

Previous Section

Next Section

Table  of Contents KSC Fact Sheets Next Page Top

Solid Rocket Booster Overpressure Suppression System is part of the Sound Suppression Water System. It alleviates the effect of a reflected pressure pulse which occurs at booster ignition. Without the suppression system, this pressure would exert significant forces on the wings and control surfaces of the orbiter.

There are two primary components to this acoustic energy suppression system. A water spray system provides a cushion of water which is directed into the flame hole directly beneath each booster. A series of water bags stretched across the flame holes, providing a water mass to dampen the reflected pressure pulse, supplements this effort. Used together, this water barrier blocks the path of the reflected pressure wave from the boosters, greatly decreasing its intensity.

In the event of an aborted mission, a Post-Shutdown Engine Deluge System will cool the aft end of the orbiter. It also controls the burning of residual hydrogen gas after the Shuttle's main engines have been shut down with the vehicle on the pad. There are 22 nozzles around the exhaust hole for the main engines within the Mobile Launcher Platform. Fed by a 6-inch-diameter (15-centimeter) supply line, water flows at a rate up to 2,500 gallons (9,463.5 liters) per minute.

  

KSC Home Page Site Search FAQ's Site Survey Customer Forum NASA Centers Privacy Statement Headlines

Page Last Revised

Page & Curator Information

08/28/2000

 Curator: Kay Grinter (kay.grinter-1@ksc.nasa.gov) / InDyne, Inc. 
Web Development: JBOSC Web Development Team
A Service of the NASA/KSC External Relations and Business Development Directorate
JoAnn H. Morgan, Director