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Viewing 1 to 30 of 83
CURRENT
1985-03-01
Standard
AIR1921
This report describes a method of semiconductor resistance measurement using controlled energy levels and a digital processing oscilloscope to acquire and process test data.
HISTORICAL
1963-07-01
Standard
AIR784
To describe typical ignition systems in general usage and their parameters that warrant considerations during the development of a gas turbine engine. To describe those parameters in gas turbine engine design and, in particular, burner configurations that influence the type selection and performance of the ignition system. To indicate the areas where future work may uncover important effects having a direct bearing on certain interrelated parameters, with resultant benefits to both the engine and ignition designers..
HISTORICAL
1984-06-01
Standard
AIR784B
To describe typical ignition systems in general usage and their parameters that warrant consideration during the development of a gas turbine engine.
HISTORICAL
1975-06-01
Standard
AIR784A
To describe typical ignition systems in general usage and their parameters that warrant consideration during the development of a gas turbine engine.
CURRENT
1995-06-01
Standard
AIR784C
To describe typical ignition systems in general usage and their parameters that warrant consideration during the development of a gas turbine engine. To describe those parameters in gas turbine engine design and, in particular, burner configurations that influence the type selection and performance of the ignition system. To indicate the areas where future work may uncover important effects having a direct bearing on certain interrelated parameters, with resultant benefits to both the engine and ignition designers.
CURRENT
1990-08-01
Standard
AIR4090
This report describes basic methods, typical results, limitations, and technical variables which may provide some relative performance expectations for different lots of the same material, or comparison characteristics for different materials. This testing alone does not assure satisfactory operation in the engine, i.e., there is not a direct relationship to actual engine performance.
CURRENT
1969-10-01
Standard
AIR1090
This report includes a procedure for typical pulse voltage measurement using the pressurized ball gap, calibration procedure, and a description of the pressurized ball gap.
CURRENT
1969-10-01
Standard
AIR1091
This report covers the use, electro-mechanical description, and accuracy of a pulse generator in the range of 5 to 30 kilovolts and zero to peak voltage time of less than 1.0 microsecond.
CURRENT
1965-03-01
Standard
AIR885
HISTORICAL
1968-06-01
Standard
AIR951
CURRENT
1998-08-01
Standard
AIR951A
Parameters to consider and various methods of measuring spark energy of aviation ignition systems.
CURRENT
1966-06-01
Standard
AIR913
This information report provides a short glossary of rocket ignition and related terms.
CURRENT
1994-06-01
Standard
AIR84A
These specifications contain general information about the characteristics of ignition systems and measuring techniques; recommended types of voltage dividers and output indicators; calibration procedures.
HISTORICAL
1959-02-01
Standard
ARP368A
HISTORICAL
1960-04-01
Standard
ARP368B
CURRENT
1972-12-04
Standard
ARP368C
CURRENT
1954-06-01
Standard
ARP295
CURRENT
1954-06-15
Standard
ARP294
CURRENT
2002-07-23
Standard
ARP296
CURRENT
1962-06-01
Standard
ARP489A
This specification establishes the requirements for shielded, detachable high tension spark plug leads for reciprocating engines.
HISTORICAL
1956-03-15
Standard
ARP489
This specification establishes the requirements for shielded, detachable high tension spark plug leads for reciprocating engines.
HISTORICAL
1976-11-15
Standard
ARP504B
This procedure establishes the ignition system power supply design parameters for aeronautical engine ignition system testing.
CURRENT
1980-04-15
Standard
ARP504C
This procedure establishes the ignition system power supply design parameters for aeronautical engine ignition system testing.
HISTORICAL
1971-06-15
Standard
ARP504A
This specification establishes the ignition system power supply design parameters for aeronautical engine ignition systems.
CURRENT
1971-07-01
Standard
ARP484A
Viewing 1 to 30 of 83