Accession Number:

AD0296560

Title:

SPECIFICATION DESIGN STUDY FOR FLIGHT TESTING INERTIAL GUIDANCE SYSTEMS GEM (GUIDANCE EVALUATION MISSILE)

Descriptive Note:

Monthly progress rept. no. 3, 22 Jan-28 Feb 1962

Corporate Author:

TRW SPACE TECHNOLOGY LABS REDONDO BEACH CA

Personal Author(s):

Report Date:

1962-03-01

Pagination or Media Count:

177.0

Abstract:

Descriptors:

• *THERMODYNAMICS
• *GUIDED MISSILE TRAJECTORIES
• *AERODYNAMIC CONFIGURATIONS
• *INERTIAL GUIDANCE
• TEMPERATURE
• CONTROL SYSTEMS
• RADAR TRACKING
• INSTALLATION
• ERRORS
• ANTENNAS
• INSTRUMENTATION
• AUTOMATIC PILOTS
• GUIDED MISSILE DETECTION
• AERODYNAMIC CONTROL SURFACES
• TELEMETER SYSTEMS
• FLIGHT TESTING
• SIMULATION
• GUIDED MISSILES
• GROUND EFFECT MACHINES
• REENTRY VEHICLES

Subject Categories:

• Guided Missile Trajectories, Accuracy and Ballistics
• Navigation and Guidance

Distribution Statement:

APPROVED FOR PUBLIC RELEASE