ENGINE INLET ANTI-ICING SUBSYSTEM SPECIFICATION. SST BOEING MODEL 2707, SUPERSONIC TRANSPORT PROGRAM. PHASE II-C REPORT

reportActive / Technical Report | Accession Number: AD0805658 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Petesch, E. R.
Author Organization(s):
BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV
Supplementary Note:
See also Rept. no. D6A10118-1, AD805659.
Pagination:
0030

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
D6A10117-1
Contract/Grant Number(s):
FA-SS-66-5
Monitor Series:
FAA
 Subject Terms
Joint Capability Areas:
JCA_6.4.1_Secure Information Exchange; JCA_4.3_Maintain; JCA_5_Command and Control; JCA_6_Net Centric; JCA_5.3_Planning; JCA_6.4_Information Assurance; JCA_JCA_4.1.2_Sustain the Force; JCA_4.1_Deployment and Distribution; JCA_3.2_Engagement; JCA_3_Force Application; JCA_5.5.2_Task; JCA_5.5_Direct; JCA_3.2.1_Kinetic Means
Communities of Interest:
Human Systems
Descriptor(s):
*JET TRANSPORT AIRCRAFT, *TURBOJET INLETS, *DEICING SYSTEMS, COMMERCIAL AIRCRAFT, NONDESTRUCTIVE TESTING, SPECIFICATIONS, PERFORMANCE(ENGINEERING), ICE PREVENTION, TURBOJET ENGINES, SUPERSONIC AIRCRAFT, AVIATION SAFETY, MAINTAINABILITY, SAFETY, QUALITY CONTROL
Field(s)/Group(s):
Civilian Aircraft, Jet and Gas Turbine Engines
Keyword(s):
BOEING 2707 AIRCRAFT, SUPERSONIC TRANSPORTS
Report Date:
1966 Jun 30