2 edition of Conceptual design studies for large free-flying solar-reflector spacecraft found in the catalog.
Conceptual design studies for large free-flying solar-reflector spacecraft
John M Hedgepeth
by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va
Written in English
|Statement||John M. Hedgepeth, Richard K. Miller, and Karl Knapp ; prepared for Langley Resarch Center|
|Series||NASA contractor report -- 3438|
|Contributions||Miller, Richard K. 1949-, Knapp, Karl, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Astro Research Corporation|
|The Physical Object|
|Pagination||ix, 110 p. :|
|Number of Pages||110|
This design study focused on exhibit and viewing areas improvements to explore the concept of landscape immersion and of a home place for gorillas in Prague Zoo. The first concept is based on wetland areas around Baji, Gabon, giving gorillas plenty of space and diverse habitats similar to the grassland, forest, and a matrix of wet areas. A space habitat (also called a space colony, space settlement, orbital habitat, orbital settlement or orbital colony) is more than a bare-bones space station, in that it is intended as a permanent settlement or green habitat rather than as a simple way-station or other specialized facility. No space habitat has been constructed yet, but many design concepts, with varying degrees of realism.
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Perhaps the same can be done for NASA spacecraft. This study will explore the concept of designing and fabricating a spacecraft based entirely on flexible substrate printed electronics. The study will consider mission requirements, manufacturing compatibility and advanced technology from both industry and . The book presents a broad view of the complete spacecraft. The objective is to explain the thought and analysis that go into the creation of a spacecraft with simplicity and with enough worked examples so that the reader can be self taught if necessary. After studying the book, readers should be able to design a spacecraft, to the phase A level Reviews: 5.
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Conceptual design studies for large free-flying solar-reflector spacecraft. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. Conceptual Design Studies for Large Free-Flying Solar-Reflector Spacecraft John M.
Hedgepeth, Richard K. Miller, and Karl Conceptual design studies for large free-flying solar-reflector spacecraft book Astro Research Corporatioll Carpinteria, Califoruia Prepared for Langley Research Center under Contract NASl NI\S/\ National Aeronautics and Space Administration Scientific and Technical.
Conceptual design studies for large free-flying solar-reflector spacecraft / By John M. Hedgepeth, Karl. Knapp, Richard K.
(Richard Keith) Miller, Astro Research Corporation., United States. National Aeronautics and Space Administration. Conceptual design studies for large free-flying solar-reflector spacecraft reflecting film surface is supported by a lightweight structure which may be automatically deployed after launch in the Space Shuttle.
A twin rotor, control moment gyroscope, with deployable rotors, is included as a primary control actuator. The structural. The design criteria for large space structures are studied. Critical baseline design requirements for general types of structures are identified by a series of rational parametric analyses.
This is for a large part due to the challenging space environment, but also to the lack of basic R&D, and to other cultural factors within the design community. On the other hand, another reason for slow space travel application design is the high energy cost, and low efficiency, for achieving orbit.
Ribble () re ports a design study for this deployable module, including conceptual assembly scenarios which include astronaut extra-vehicular activity (EVA) and Shuttle attached or free-flying assembly fixtures.
This study details initial joint hardware designs as well as parametric performance estimates, shown in Fig. 12, of antenna. This book is drawn from the author's years of experience in spacecraft design, culminating in his leadership of the Magellan Venus orbiter spacecraft design from concept through launch.
The book also benefits from his years of teaching spacecraft design at University of Colorado at Boulder and from its use as a popular home study short course.
A space elevator is a proposed type of planet-to-space transportation system. The main component would be a cable (also called a tether) anchored to the surface and extending into design would permit vehicles to travel along the cable from a planetary surface, such as the Earth's, directly into space or orbit, without the use of large rockets.
A concept image of a spacecraft powered by a fusion-driven rocket. In this image, the crew would be in the forward-most chamber. Solar panels on the sides would collect energy to. Free-flying space manipulator systems, in which robotic manipulators are mounted on a free-flying spacecraft, are envisioned for assembling, maintenance, repair, and contingency operations in space.
Nevertheless, even for fixed-base systems, control of mechanical manipulators is a challenging task. Free-flying space manipulator systems, in which robotic manipulators are mounted on a free-flying spacecraft, are envisioned for assembling, maintenance, repair, and contingency operations in space.
Nevertheless, even for fixed-base systems, control of. The Advanced Concepts Office at Marshall Space Flight Center completed a brief spacecraft design study for the 8-meter monolithic Advanced Technology Large Aperture Space Telescope (ATLAST-8m).
This spacecraft concept provides all power, communication, telemetry, avionics, guidance and control, and thermal control for the observatory.
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Space Mission Engineering: The New SMAD (Space Technology Library, Vol. 28)Reviews: 6. The Reference Mission spacecraft would take astronauts to Mars in about days.
"Our advanced designs, like the gas core and the ablative engine concepts, could take astronauts to Mars in half that time, and perhaps even in as little as 45 days," said Kirby Meyer, an engineer with Positronics Research on the study.
The designer should be aware of design guidelines to avoid surface and internal charging problems (Sections and ). All guidelines should be considered in the spacecraft design and applied appropriately to the given mission. Analysis. Analysis should be used to evaluate a design for charging in the specified orbital environment.
NASA Goddard Space Flight Center Mission Design Processes (The "Green Book") [PDF; Kb, 54 pgs.] Systems Interfaces Safety Documents. Safety Policy and Requirements for Payloads using the Space Transportation System - NSTS B - Space Shuttle Program, Jan. [PDF; 64 pgs, Mb] Launch Vehicle Documents.
Project Daedalus is a concept design for an interstellar probe, developed in the s by a group of technical specialists for the British Interplanetary Society. project was the design of the. Annotation This new book is drawn from the author's years of experience in spacecraft design, culminating in his leadership of the Magellan Venus orbiter spacecraft design from concept through launch.
The book also benefits from his years of teaching spacecraft design at University of Colorado at Boulder and as a popular home study short course for s: 1. Reflector/Shades a flexible solar reflector and shade design. Some projects from the Book "Low Cost Solar Heating -- Daring Schemes Tried and Untred", William Shurcliff.
Three -Mode Reflecting and insulatiing plates for use the Bier's Absorber and Storage Walls. These are conceptual design layout drawings, sketches, and model photos of examples of the earliest stages of aircraft design.
Most of these were never built - we typically design hundreds of aircraft concepts at the "conceptual" level for every one that ever actually flies.
Thanks to Lockheed, Rockwell, AIAA, and others for making these available.American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA The study investigated a two-stage liquid propulsion concept, an optimized MAV trajectory, guidance, navigation, and control, thermal requirements, MAV components, and MAV support systems.