Applications for large deployable antennas were re-examined, flight demonstration objectives were defined, the flight article (antenna) was preliminarily designed, and the flight program and ground development program, including the support equipment, were defined for a proposed space transportation system flight experiment to demonstrate a large (50 to 200 meter) deployable antenna system. Tasks described include: (1) performance requirements analysis; (2) system design and definition; (3) orbital operations analysis; and (4) programmatic analysis
Photographic summary report of Lunar Orbiter 4 mission. The fourth of five Lunar Orbiter spacecraft ...
This document is the response to the National Space Policy Directive-4 (NSPD-4), signed by the Presi...
Pratt & Whitney (P and W) is currently under contract to NASA-LeRC for a multi-year program to evalu...
The development of a laser altimeter for use in the Apollo Lunar Orbital Experiments mission is disc...
Developing structure, payload, communication and data handling subsystems for ERT
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
The crew capsule of the MOTV was studied with emphasis on crew accommodations, crew capsule function...
A concept for an orbiting laboratory for testing Controls-Structures Integration (CSI) technology is...
The Integrated Receiver/Decoder (IRD) currently used on the Space Shuttle was designed in the 1980 a...
The Advanced Information Processing System (AIPS) is a fault-tolerant distributed computer system ar...
A series of flight tests were conducted to collect data for jet transport aircraft flying curved-pat...
The three NASA/USAF lunar probes of August 17, October 13, and November 8, 1958 are described. Detai...
Flight test program to obtain data on aided inertial system for terminal guidance and navigation of ...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
The Terminal Configured Vehicle (TCV) program operates a Boeing 737 modified to include a second coc...
Photographic summary report of Lunar Orbiter 4 mission. The fourth of five Lunar Orbiter spacecraft ...
This document is the response to the National Space Policy Directive-4 (NSPD-4), signed by the Presi...
Pratt & Whitney (P and W) is currently under contract to NASA-LeRC for a multi-year program to evalu...
The development of a laser altimeter for use in the Apollo Lunar Orbital Experiments mission is disc...
Developing structure, payload, communication and data handling subsystems for ERT
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
The crew capsule of the MOTV was studied with emphasis on crew accommodations, crew capsule function...
A concept for an orbiting laboratory for testing Controls-Structures Integration (CSI) technology is...
The Integrated Receiver/Decoder (IRD) currently used on the Space Shuttle was designed in the 1980 a...
The Advanced Information Processing System (AIPS) is a fault-tolerant distributed computer system ar...
A series of flight tests were conducted to collect data for jet transport aircraft flying curved-pat...
The three NASA/USAF lunar probes of August 17, October 13, and November 8, 1958 are described. Detai...
Flight test program to obtain data on aided inertial system for terminal guidance and navigation of ...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
The Terminal Configured Vehicle (TCV) program operates a Boeing 737 modified to include a second coc...
Photographic summary report of Lunar Orbiter 4 mission. The fourth of five Lunar Orbiter spacecraft ...
This document is the response to the National Space Policy Directive-4 (NSPD-4), signed by the Presi...
Pratt & Whitney (P and W) is currently under contract to NASA-LeRC for a multi-year program to evalu...