Accession Number:

AD0364763

Title:

TITAN III/MOL 156-INCH SOLID ROCKET MOTOR DESIGN CONSTRAINTS REPORT (THREE CENTER SEGMENTS)

Descriptive Note:

Corporate Author:

MARTIN CO DENVER COLO

Personal Author(s):

Report Date:

1965-08-31

Pagination or Media Count:

196.0

Abstract:

This document establishes the restraints and criteria for the design and test of an improved Stage O to be used with the Titan IIIMOL booster. The new Stage O involves three system segments. These are two identical new 156-inch diameter solid rocket motors, the auxiliary equipment and subsystems necessary to integrate these motors to the existing Titan III core, and the AGE for on-pad assembly and checkout of this stage at the Initial Launch Capability ILC facility at AFWTR. Author

Descriptors:

• *LAUNCH VEHICLES
• *SOLID PROPELLANT ROCKET ENGINES
• SOLID PROPELLANT ROCKET ENGINES
• MANNED SPACECRAFT
• AERONAUTICAL LABORATORIES
• PERFORMANCE(ENGINEERING)
• MAINTENANCE
• RELIABILITY
• VIBRATION
• NOISE
• GROUND SUPPORT EQUIPMENT
• MATERIALS
• STRUCTURAL PROPERTIES
• LOAD DISTRIBUTION
• THRUST
• THRUST VECTOR CONTROL SYSTEMS
• HYDRAULIC EQUIPMENT
• DEFLECTION
• CONFIGURATIONS
• STAGING
• ACCELERATION
• AERODYNAMIC HEATING
• TRAJECTORIES
• QUALITY CONTROL

Subject Categories:

• Solid Propellant Rocket Engines
• Ground Support Systems and Facilities for Space Vehicles
• Manned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE