(Sanitized)

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP63-00313A000600010009-6
Release Decision: 
RIPPUB
Original Classification: 
S
Document Page Count: 
2
Document Creation Date: 
December 14, 2016
Document Release Date: 
August 9, 2002
Sequence Number: 
9
Case Number: 
Publication Date: 
May 2, 1958
Content Type: 
MEMO
File: 
AttachmentSize
PDF icon CIA-RDP63-00313A000600010009-6.pdf35.91 KB
Body: 
Approved For Release SEC ',r CIA-RDP6'3'6031 p00600010009-6 CHAL - 0045 Copy of 5 2 May 1955 MEmCRANDUM TO: Deputy Project Director 25X1 A SUBJECT 25X1 A 1. The following information was elicited from this date. As pertains to the J-57/P31 Engine: T.O. 35,000 70,Q A. Specific Fuel Consumption 1.06 .95 1.13 B. Mass Air Flow 234#/sec 75#/sec 13#/sec' C. Thrust 14,600, 3750 655-. D. Compression Ratio 13.1 13.1 13:1 E. Engine Basic Weight Thrust at 3700 37 3700 atd Altitudes; F. Fuel Consumption and (1) Sea Level a. Thrust b. 1.06 Fuel Consumption (2) 15,000 Feet a. 7,000 Thrust b. 1.015 Fuel Consumption (3) 25,000 Feet a. 5350 Thrust b. 1.00 Fuel Consumption (4) 35,000 Feet a. 3750 Thrust b. .95 Fuel Consumption G. Turbine Inlet Temperature (2 (3 Take Off - 1670?F 35,000 Feet - 1670?F 70,000 Feet - 1670?F Approved For Release 2002/10/23EG P63-0J0313A000600010009-6 -4./ Approved For Release 2002/1ST"~1 I RDP63-OM 3A0000600010009-6 CHAL - 0045 Page two of two 25X1A Approved For Release 2002/1050 1RDP63-00313A000600010009-6