SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE 3. PROPOSAL. BOEING MODEL 2707. VOLUME 2-6-1. AIRFRAME DESIGN REPORT. PART A. WEIGHT AND BALANCE

reportActive / Technical Report | Accession Number: AD0804726 | Open PDF

Abstract:

This report gives a detail weight breakdown of the proposed airplane and the design data and methods used in determining these weights. The report also includes moment of inertia, balance, and loading information. Supplement A provides weight data for the prototype airplane and Supplement B provides data for the domestic.

Author(s):
Brown, E. M.
Author Organization(s):
BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV
Supplementary Note:
See also Volume 2. AD804727.
Pagination:
0114

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
V2-B2707-6-1
Contract/Grant Number(s):
FA-SS-66-5
Monitor Series:
FAA
 Subject Terms
Joint Capability Areas:
JCA_6_Net Centric; JCA_6.4.1_Secure Information Exchange; JCA_6.1.1_Wired Transmission; JCA_4.1_Deployment and Distribution; JCA_6.1.3_Switching and Routing; JCA_6.1_Information Transport; JCA_5_Command and Control; JCA_4_Logistics; JCA_6.4_Information Assurance; JCA_4.5.4_Requirements Definition; JCA_4.5_Operational Contract Support; JCA_1.2_Force Preparation; JCA_1_Force Support; JCA_5.3_Planning; JCA_8.2.1_Partner with Governments and Institutions; JCA_8.2_Shape; JCA_8_Building Partnerships; JCA_JCA_4.1.2_Sustain the Force; JCA_3.2_Engagement; JCA_3_Force Application; JCA_1.2.6_Concepts
Communities of Interest:
Air Platforms
Descriptor(s):
*AIRFRAMES, *SUPERSONIC AIRCRAFT, FUEL SYSTEMS, LOADS(FORCES), DIFFUSION BONDING, WEIGHT, FATIGUE(MECHANICS), TOLERANCES(MECHANICS), WINGS, HYDRAULIC EQUIPMENT, MOMENT OF INERTIA
Field(s)/Group(s):
Transport Aircraft
Keyword(s):
*JET TRANSPORT PLANES, BOEING 2707 AIRCRAFT, SUPERSONIC TRANSPORTS, COMMUNICATION SYSTEMS
Report Date:
1966 Sep 06