Optical technology Apollo extension system, phase A, volume 3, section 3 - Experiments Final technical report
Stellar oriented and large optics experiments of optical technology development program for Apollo extension system
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Apollo guidance, navigation and control: Guidance system operations plan for manned CM earth orbital and lunar missions using Program COLOSSUS 3. Section 3: Digital autopilots (revision 14)
Digital autopilots for the manned command module earth orbital and lunar missions using program COLOSSUS 3 are discussed. Subjects presented are: (1) reaction control system digital autopilot, (2) thrust vector control autopilot, (3) entry autopilot and mission control programs, (4) takeover of Saturn steering, and (5) coasting flight attitude maneuver routine.
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Documentation for the machine-readable version of A Finding List for the Multiplet Tables of NSRDS-NBS 3, Sections 1-10 (Adelman, Adelman, Fischel and Warren 1984)
The machine-readable finding list, as it is currently being distributed from the Astronomical Data Center, is described. This version of the list supersedes an earlier one (1977) containing only Sections 1 through 7 of the NSRDS-NBS 3 multiplet tables publications. Additional sections are to be incorporated into this list as they are published.
Warren, W. H., Jr.↗
Lecture notes in economics and mathematical system. Volume 150: Supercritical wing sections 3
Application of computational fluid dynamics to the design and analysis of supercritical wing sections is discussed. Computer programs used to study the flight of modern aircraft at high subsonic speeds are listed and described. The cascades of shockless transonic airfoils that are expected to increase the efficiency of compressors and turbines are included.
Bauer, F.↗
Guidance system operations plan for manned cm earth orbital and lunar missions using program Colossus 3. Section 2: Data links
The data links for use with the guidance system operations plan for manned command module earth orbital and lunar missions using program Colossus 3 are presented. The subjects discussed are: (1) digital uplink to CMC, (2) command module contiguous block update, (3) CMC retrofire external data update, (4) CMC digital downlink, and (5) CMC entry update.
Hamilton, M. H.↗
Apollo guidance, navigation and control: Guidance system operations plans for manned LM earth orbital and lunar missions using Program COLOSSUS 3. Section 7: Erasable memory programs
Erasable-memory programs (EMPs) designed for the guidance computers used in the command (CMC) and lunar modules (LGC) are described. CMC programs are designated COLOSSUS 3, and the associated EMPs are identified by a three-digit number beginning with 5. LGC programs are designated LUMINARY 1E, and the associated EMPs are identified, with one exception, by a three-digit number beginning with 1. The exception is EMP 99. The EMPs vary in complexity from a simple flagbit setting to a long and intricate logical structure. They all, however, cause the computer to behave in a way not intended in the original design of the programs; they accomplish this off-nominal behavior by some alteration of erasable memory to interface with existing fixed-memory programs to effect a desired result.
Hamilton, M. H.↗
MINNEAPOLIS. ADAPTIVE STATE VECTOR CONTROL. SECTION 3- MEASUREMENT OF THE STATE VECTOR
Measurement of the state control vector
VECTOR CONTROL↗
Optical Technology Apollo Extension System, Part I. Volume II. Section 3 - Systems Integration Final Technical Report
Systems integration for Optical Technology Apollo Extension System
OPTICAL INSTRUMENT↗
Optical technology Apollo extension system, phase A, volume 2. Section 3 - Experiments
Optical propagation in turbulent atmosphere, optical communication diagnostics, spaceborne heterodyne experiments, and ground support requirements
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Compendium of Human Responses to the Aerospace Environment. Volume 3 - Sections 10-16
Human responses to spacecraft cabin atmosphere, pressure, and contamination, and water supply, diet, and anthropometry
Roth, E. M.↗
Hypersonic cruise vehicle wing structure evaluation - Volume 3, sections 23-27
Cost, performance, reliability, interaction, and structural element analyses for hypersonic cruise vehicle wings
Davis, G. W.↗
Radiation effects design handbook. Section 3 - Electrical insulating materials and capacitors
Steady state radiation effects on electrical insulating materials and capacitors - handbook
Hamman, D. J.↗
Modular space station detailed preliminary design. Volume 3: Sections 4.9 through 6
For abstract, see N72-21880.
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Guidance system operations plan for manned CSM earth orbital and lunar missions using program COLOSSUS 3. Section 7: Erasable memory programs
Erasable-memory programs designed for guidance computers used in command and lunar modules are presented. The purpose, functional description, assumptions, restrictions, and imitations are given for each program.
Hamilton, M. H.↗
Operators manual for microdensitometer control program densitometer model PDS-1010G (modified). Program trace version 3B (section 3)
The PDS-1010G microdensitometer is run under the control of a PDP-11 program called TRACE. This program gives the operator vary flexible control over the machine functions. Most commands are passed to the computer through either the Tektronix 4010 terminal or the teletype, as selected by the position of the LOCAL/LINE rocker switch above the 4010 keyboard. (LINE places the 4010 in control; LOCAL transfers control to the teletype. In general, the teletype is used when the operator desires a permanent record of the operator-computer dialogue.) A small number of control functions are requested by setting switches on the computer front panel.
Title, A. M.↗
Systems design study of the Pioneer Venus spacecraft. Appendices to volume 1, sections 3-6 (part 1 of 3)
The design is described of the Venus probe windows, which are required to measure solar flux, infrared flux, aureole, and cloud particles. Window heating and structural materials for the probe window assemblies are discussed along with the magnetometer. The command lists for science, power and communication requirements, telemetry sign characteristics, mission profile summary, mass properties of payloads, and failure modes are presented.
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Microwave power transmission system studies. Volume 3, section 8: Mechanical systems and flight operations
The efforts and recommendations associated with preliminary design and concept definition for mechanical systems and flight operations are presented. Technical discussion in the areas of mission analysis, antenna structural concept, configuration analysis, assembly and packaging with associated costs are presented. Technology issues for the control system, structural system, thermal system and assembly including cost and man's role in assembly and maintenance are identified. Background and desired outputs for future efforts are discussed.
Maynard, O. E.↗
The large motor plume/material impingement test program at AEDC utilizing the four selected propellants from the small motor tests at MSFC (July, August, and September 1974), section 3
Efforts made to determine the vulnerability of Orbiter and ET materials located at various positions within exhaust plumes from test SSRM's using four different propellant formulations are discussed. Data also cover the effect on TPS materials from a single SSRM plume and dual SSRM plumes, and definitions of test SSRM plume environment at material specimen locations.
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