Accession Number:

AD0668246

Title:

THE SHOCK AND VIBRATION BULLETIN 37, PART 5

Descriptive Note:

Corporate Author:

NAVAL RESEARCH LAB WASHINGTON DC SHOCK AND VIBRATION INFORMATION CENTER

Personal Author(s):

Report Date:

1968-01-01

Pagination or Media Count:

184.0

Abstract:

Contents Vibroacoustic environmental simulation for aerospace vehicles RTD sonic fatigue facility, design and performance characteristics Operational characteristics of a 100,000-cubic-foot acoustic reverberation chamber Concept, design, and performance of the spacecraft acoustic laboratory Theoretical study of acoustic simulation of in-flight environments Data handling methods for large vehicle testing Development and verification of the vibration test requirements for the Apollo command and service modules Development and verification of the Apollo lunar module vibration test requirements Saturn S-II, S-IVB, and instrument unit subassembly and assembly vibration and acoustic evaluation programs Development of acoustic test conditions for Apollo lunar module flight certification Facility sonic fatigue proof testing Vibroacoustic test methods for vibration qualification of Apollo flight hardware Acoustical qualification of S-IC fin structures Simulation of acoustic fatigue failure in the wideband noise test facility of the Air Force Flight Dynamics Laboratory Real-time combined acoustic-vacuum testing of spacecraft.

Subject Categories:

  • Helicopters
  • Information Science
  • Mechanics
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE