Accession Number:

AD0423703

Title:

STANDARD LAUNCH VEHICLE I (SLV-I) SYSTEM DESCRIPTION AND OPERATION SUMMARY,

Descriptive Note:

Corporate Author:

AEROSPACE CORP EL SEGUNDO CALIF

Personal Author(s):

Report Date:

1963-09-01

Pagination or Media Count:

169.0

Abstract:

An SLV-I system description and flight operation summary is presented for ready reference to the SLV-I program and to facilitate reliability evaluations. The system description is brief and primarily concerned with defining configuration differences. The flight operation summaries are extracts of system hardware performance and anomalies as reported in contractor flight evaluation reports. The SLV-I is an inexpensive, diversified missile used for space exploration. Basic configurations of SLV-I used are LV-1B, threestage unguided SLV-IB, four-stage unguided BSI, three-stage guided BSII, four-stage guided and SLV-IA, four-stage guided. Various payload requirements can be met by utilizing available motors. Flight histories, diagrams, charts, schematics, and tables are included. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE