DESIGN STUDY OF AN INTEGRATED AIRBORNE TELEMETRY SYSTEM

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Abstract:

The rocket telemeter study program was completed in the following phases of work 1 determination of accuracy and data requirements, 2 theoretical analysis of modulation methods, 3 comparative analysis of system capabilities, 4 survey of flight test range facilities, 5 preliminary system design, 6 component development and breadboard testing, and 7 feasibility model fabrication, test and delivery. New approaches to system and component design were required. The completed feasibility rocket telemeter system design represents a state-of-the-art advancement in an extremely compact, accurate and efficient telemetry system of high data capability. It is believed that this study program resulted in the development of the first 400 mw, true FM, all transistor transmitter. Author

Author(s):
Pruss, Hugh
Author Organization(s):
TELEMETERING CORP OF AMERICA SEPULVEDA CALIF
Pagination:
0001

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
ER 707
Contract/Grant Number(s):
DA28 017 501ORD3577
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_4.6.1_General Engineering; JCA_4.6_Engineering; JCA_3.2.1_Kinetic Means
Modernization Areas:
Microelectronics
Communities of Interest:
Weapons Technologies
Descriptor(s):
*ROCKETS, *TELEMETER SYSTEMS, *TELEMETERING TRANSMITTERS, AIRBORNE, AMPLIFIERS, CALIBRATION, CIRCUITS, CONTAINERS, CRYSTAL OSCILLATORS, DATA TRANSMISSION SYSTEMS, FREQUENCY MODULATION, MIXER TUBES, MULTIPLEXING, POWER AMPLIFIERS, RADIOFREQUENCY AMPLIFIERS, TRANSISTORS, VERY HIGH FREQUENCY
Report Date:
1960 Aug 01