Effective Ratio of Specific Heats(chamber) 1.16 (NoZzle Exit) 1.21 CURRENT STATUS Production BC1355B4/91 2000 TIME sec Star 13 B TE-M-763 148-KS-1,708 Orbit Insertion Motor 13.57 DIA 802 25.11 16.522, Space P pessan Lecture 9 Prof. Manuel martinez Page 3 of 3Effective Ratio of Specific Heats (chamber) 1.16 (Nozzle Exit) 1.21 CURRENT STATUS Production BC1355B 4/91 16.522, Space Propulsion Lecture 9 Prof. Manuel Martinez-Sanchez Page 3 of 3