The performance and operational characteristics of the J71-A2 turbojet-engine afterburner were investigated for a range of altitudes from 23,000 to 60,000 feet at a flight Mach number of 0,9 and at flight Mach numbers of 0.6, 0.9, and 1.0 at an altitude of 45,000 feet. The combustion performance and altitude operational limits, as well as the altitude starting characteristics have been determined.
Preliminary Altitude Performance Data of J71-A2 Turbojet Engine Afterburner
1954-10-07
Miscellaneous
No indication
English
Turbojet afterburning without afterburner
Engineering Index Backfile | 1950
|PRELIMINARY DESIGN OF A SHORT AFTERBURNER FOR SINGLE-SPOOL EXPENDABLE TURBOJET ENGINE
British Library Conference Proceedings | 2011
|