Accession Number:

AD0829593

Title:

WEIGHT AND BALANCE STATUS REPORT XSM-65D-IOC ISSUE NO. 4, GUIDED MISSILE,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1958-05-01

Pagination or Media Count:

22.0

Abstract:

The principal current weight changes reported herein for the Sustainer are due to 1 Aft Bulkhead Skins revised estimate -40 lbs., 2 Thrust Cone design change from steel to aluminum -33 lbs., 3 Battery and Inverter Package added to A.P.S. Backup System 134 lbs., and 4 GOX in LO2 tank revised estimate based on Aerophysics Rep. ZJ-7-053 115 lbs.. For the Booster, the principal current weight changes are due to 1 Booster Turbine Exhaust Support revised estimate based on addition of exhaust per E.W.O. 038000 30 lbs., 2 Tank Pressure System revised weight 69 lbs. and 3 Control Pressure System revised weight -45 lbs.. Author

Subject Categories:

  • Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE