WEIGHT AND BALANCE STATUS REPORT XSM-65D-IOC ISSUE NO. 4, GUIDED MISSILE,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1958
- Accession Number
- AD0829593
Entities
People
- J. M. Allenson
Organizations
- General Dynamics