The automatic beam builder ABB was developed, fabricated, and demonstrated within the established contract cost and schedule constraints. The ABB demonstrated the feasibility of: producing lightweight beams automatically within the required rate of 1 to 5 ft of completed beam per minute and producing structurally sound beams with axial design load of 5538 N based on the Grumman photovoltaic satellite solar power system design reference structure
Technologies for EVA and remote manipulation systems - handbook for systems designer
The Advanced Information Processing System (AIPS) is a fault-tolerant distributed computer system ar...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
The development of a laser altimeter for use in the Apollo Lunar Orbital Experiments mission is disc...
An investigation being conducted by Astro Aerospace Corporation (Astro) for Jet Propulsion Laborator...
Developing structure, payload, communication and data handling subsystems for ERT
The various programs involved in the development of the Skylab Orbital Workshop are discussed. The s...
Systems analysis and integration, boom subsystem, combination passive damper, and attitude sensor sy...
The beam builder, designed and manufactured as a ground demonstration model, is a precursor to a mac...
Voyager spacecraft to be launched by Titan III C launch vehicle for Mars and Venus probe - communica...
A conceptual design and program plan for an Orbital Construction Demonstration Article (OCDA), that ...
Flight dynamics, experiment operational phase sequence, and support operations for Applications Tech...
Missions for future orbit transfer vehicles (1995-2010) are identified and the technology, operation...
Application Technology Satellite /ATS/ SPACECRAFT tradeoff and analysis - configuration paraboloid a...
Parametric models were constructed for Earth-based laser powered electric orbit transfer from low Ea...
Technologies for EVA and remote manipulation systems - handbook for systems designer
The Advanced Information Processing System (AIPS) is a fault-tolerant distributed computer system ar...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
The development of a laser altimeter for use in the Apollo Lunar Orbital Experiments mission is disc...
An investigation being conducted by Astro Aerospace Corporation (Astro) for Jet Propulsion Laborator...
Developing structure, payload, communication and data handling subsystems for ERT
The various programs involved in the development of the Skylab Orbital Workshop are discussed. The s...
Systems analysis and integration, boom subsystem, combination passive damper, and attitude sensor sy...
The beam builder, designed and manufactured as a ground demonstration model, is a precursor to a mac...
Voyager spacecraft to be launched by Titan III C launch vehicle for Mars and Venus probe - communica...
A conceptual design and program plan for an Orbital Construction Demonstration Article (OCDA), that ...
Flight dynamics, experiment operational phase sequence, and support operations for Applications Tech...
Missions for future orbit transfer vehicles (1995-2010) are identified and the technology, operation...
Application Technology Satellite /ATS/ SPACECRAFT tradeoff and analysis - configuration paraboloid a...
Parametric models were constructed for Earth-based laser powered electric orbit transfer from low Ea...
Technologies for EVA and remote manipulation systems - handbook for systems designer
The Advanced Information Processing System (AIPS) is a fault-tolerant distributed computer system ar...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...