NOZZLE OF A JET ENGINE,

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Abstract:

The object of the invention is a jet engine nozzle, characterized by the fact that for the purpose of gaining the possibility of controlling the thrust vector in vertical plane, it is provided with a turning-in-vertical-plane fitting, mounted on thrust bearings and work gear coupled with drive mechanism. Author

Author(s):
Shulikov, K. V.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Unedited rough draft trans. of Russian patent 166 244, appl. 10682/350455/40-23, 18 Dec 46, 2p.
Annotation:
Translation of a Russian patent: jet engine nozzle for thrust vector control.
Pagination:
0006

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-TT-65-782, TT-65-64157
Monitor Series:
65-64157
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
*THRUST VECTOR CONTROL SYSTEMS, TURBOJET EXHAUST NOZZLES, PATENTS, JET ENGINES, USSR
Report Date:
1965 Sep 22