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Successful development of an aircraft with vertical landing capability must address the critical problem of balancing the aircraft for hover. In this paper a parametric method for balancing short takeoff and vertical landing (STOVL) aircraft in hover is described and applied to the analysis of two conceptual STOVL fighters. One uses a remote augmented lift system and the other a thrust-vectoring hybrid tandem-fan engine.

Animal research on the Space Station presents the need for bioisolation, which is here defined as instrumental and operational provisions, which will prevent the exchange of particles greater than 0.3 μ size and microorganisms between crew and animals. Current design principles for the Biological Research Project thus call for: 1. use of specific pathogen-free animals; 2. keeping animals at all times in enclosed habitats, provided with microbial filters and a waste collection system; 3. placing habitats in a holding rack, centrifuge, and workbench, all equipped with particulate and odor filters, 4. washing dirty cage units in an equipment cleaner, with treatment and recycling of the water; 5. designing components and facilities so as to ensure maximal accessibility for cleaning; 6. defining suitable operational procedures. Limited ground tests of prototype components indicate that proper bioisolation can thus be achieved.

New aircraft technologies are presented that have the potential to expand the air transportation system and reduce congestion through new operating capabilities while also providing greater levels of safety and environmental compatibility. These new capabilities will result from current and planned civil aeronautics technology at the NASA Ames, Lewis, and Langley Research Centers and will cover the complete spectrum of current aircraft and new vehicle concepts including rotorcraft (helicopters and tilt rotors), vertical and short takeoff and landing (V/STOL) and short takeoff and landing (STOL) aircraft, subsonic transports, high-speed transports, and hypersonic/transatmospheric vehicles. New technologies will improve efficiency, affordability, safety, and environmental compatibility of current aircraft and will enable the development of new vehicles that could revolutionize or greatly change the transportation system.

Results of a substantial body of ground-based simulation experiments indicate that a high degree of precision of operation for recovery aboard small ships in heavy seas and low visibility with acceptable levels of effort by the pilot can be achieved by integrating the aircraft flight and propulsion controls. The availability of digital fly-by-wire controls makes it feasible to implement an integrated control design to achieve and demonstrate in flight the operational benefits promised by the simulation experience. It remains to validate these systems concepts in flight to establish their value for advanced short takeoff vertical landing (STOVL) aircraft designs.

The Advanced Programs Office at NASA Ames Research Center has defined hypothetical experiments for a 90-day mission on Space Station to allow analysis of the materials necessary to conduct the experiments and to assess the impact on waste processing of recyclable materials and storage requirements of samples to be returned to earth for analysis as well as of non-recyclable materials. The materials include the specimens themselves, the food, water, and gases necessary to maintain them, the expendables necessary to conduct the experiments, and the metabolic products of the specimens. This study defines the volumes. flow rates, and states of these materials, Process concepts for materials handling will include a cage cleaner, trash compactor, biological stabilizer, and various recycling devices.

The Advanced Programs Office in the Life Sciences Division at Ames has performed a survey and analysis of hardware and operational requirements necessary for supporting plant and animal research onboard the Space Station. This research may be conducted internal to a dedicated pressurized module, distributed among several modules, and on external platforms and free flyers. Hypothetical experiments have been defined and integrated into 90 day missions to allow analysis of crew activities and timelines, resource requirements (e.g. power, weight, and volume), equipment layouts, and alternative levels of equipment automation. Where these analyses have shown critical areas for automation, conceptual designs have been developed to evaluate feasibility. To stay within current Space Station resource allocations, approximately 85% of the planned life science experiment tasks must be automated.

A Life Sciences Research Facility on a Space Station will contribute to the health and well-being of humans in space, as well as address many fundamental questions in gravitational and developmental biology. Scientific interests include bone and muscle attrition, fluid and electrolyte shifts, cardiovascular deconditioning, metabolism, neurophysiology, reproduction, behavior, drugs and immunology, radiation biology, and closed life-support system development. The life sciences module will include a laboratory and a vivarium.

Work completed to date within the NASA CELSS program suggests that the technologies needed for growing plants in the space environment are sufficiently well understood to allow an early application that would enhance the quality of life for the crew while they are in space. Specifically, the growth of salad vegetables on Space Station Freedom, and during other long duration missions, can provide psychological and dietary benefits to crewmembers. For this reason, a unit capable of producing 600 grams of edible salad vegetables, enough for one salad three times a week for a crew of four is being planned at the NASA Ames Research Center with the involvement of university scientists and engineers. Although the growth requirements for specific plants are well established, providing these requirements within the constraints of the space environment will demand preliminary space flight tests of selected technologies, and of some plant growth behaviors.

In this paper we present a Vertical Situation Display (VSD) for Flight Management System equipped aircraft. It was developed, implemented and evaluated in the Advanced Concepts Flight Simulator at NASA Ames Research Center. The VSD was designed to support flight crews in managing the vertical flight path when using high levels of aircraft automation inside Terminal Areas.

Advanced aircraft configurations offer new transportation options for the Pacific Basin. This paper describes a range of vehicles from low-disk to high-disk loading aircraft, including high-speed rotorcraft, subsonic vertical and short takeoff and landing (V/STOL) aircraft, and subsonic short takeoff and landing (STOL) aircraft. The status and advantages of the various configurations are described. Some of these configurations show promise for satisfying many of the transportation requirements of the Pacific Basin; as such, they could revolutionize short-haul transportation in that region.