首页> 美国政府科技报告 >VOLUME 2 OF 2 AN INVESTIGATION OF THE 0.0091 SCALE EXTERNAL TANK OGIVE HOSE (MSFC MODEL 470) IN THE MSFC 14 INCH TWT TO DETERMINE THE PRESSURE DISTRIBUTION AROUND THE EXTERNAL TANK HOSE (TA3F)
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VOLUME 2 OF 2 AN INVESTIGATION OF THE 0.0091 SCALE EXTERNAL TANK OGIVE HOSE (MSFC MODEL 470) IN THE MSFC 14 INCH TWT TO DETERMINE THE PRESSURE DISTRIBUTION AROUND THE EXTERNAL TANK HOSE (TA3F)

机译:第2卷第2期对msFC 14英寸的0.0091尺度外部罐体软管(msFC 470型)进行调查,以确定外部罐体软管周围的压力分布(Ta3F)

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A wind tunnel pressure test of the Space Shuttle External Tank Nose, TWT 609, was conducted in the MSFC 14" by 14" frisonic wind tunnel during October of 1974. Tilted model was a 0.0091 scale representation of the olives nose section of the External Tank with nose cap and lightning rod and protuberances. The designation HSFC model #470 has been assigned to the in del and its support hardware. The NASA test series number is TA3F. The primary purpose of the test was to determine the pressure distribution around the nose cap. Pressure data were also obtained along the give nose.

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