Preliminary studies of possible cosmic dust impacts on project mercury vehicle periscope lenses.
Craters on flown Mercury vehicle periscope lenses possibly due to cosmic dust impacts
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Craters on flown Mercury vehicle periscope lenses possibly due to cosmic dust impacts
Transonic dynamic stability characteristics of Mercury capsule scale model configurations
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Afterbody heating by Mercury spacecraft during reentry determined from skin temperatures
Full-scale flight test from sea level of abort- escape system for manned Mercury capsule
Compilation of wind-tunnel heat-transfer measurements on afterbody of Mercury capsule reentry configuration
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Review of endocrine control of fluid and electrolyte balance during Mercury, Gemini, and Apollo missions
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This report contains the results of a preliminary study of the search and. recovery operations required. for the safe and. expeditious return of the Mercury Recovery Capsule in the first series of orbital flights. The study is concerned primarily with the high-probability impact areas in the Atlantic Ocean. Emphasis is placed on safe recovery within reasonable time at least cost. A preliminary study of this nature is not able to provide final answers to all of the problems; the report instead constitutes a "first look" at the overall operation. Much of the report is therefore devoted to basic data, the building blocks from which recovery systems can be assembled and evaluated. These include the performance characteristics, reliability, and cost of the vehicles and equipment which may be used, and their compatibility with one another, with the capsule, and with the expected environment. The availability of vehicles and equipment has also been considered., although it is appreciated. that this may change from week to week where the forces are drawn from the military services. consideration of alternative vehicles, equipments, and systems, and their evaluation from the standpoint of effectiveness and. cost. While the equipment considered. is generally expected to be operational throughout 1960, consideration is also given to more advanced schemes which might effect reductions in recovery time, cost, or dependence upon the military forces.
On 10 June 1961, 33 tests of the aerodynamic response of the McDonnell model Mercury capsule were conducted. Variables included spin, different parachute tethers, and the addition of baffles.
No abstract available
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Mercury-Redstone project development history, and contributions to future manned spacecraft design and operation
An overview of NASA's manned space programs - the X-I5, Project Mercury, Project DynaSoar, Project Gemini, and Project Apollo.
The primary mission report includes the Venus encounter and the first Mercury encounter. Plans and activities undertaken to successfully achieve the mission objectives are described. Operational activities are identified by mission operation system functions, providing a brief summary of each discipline. Spacecraft performance is summarized by subsystems.
The Mariner Venus/Mercury 1973 mission operations Extended Mission is described. The activities are summarized from shortly after Mercury I through the end of mission. The operational activities are reported by Mission Operations Systems functions providing a brief summary from each discipline. Based on these experiences recommendations for future projects are made.
Space feeding concept for Gemini and Apollo projects as developed in Mercury project