OPERATIONS - FLIGHT CREW REQUIREMENTS
Flight simulation in crew training - manned space flight
MANNED SPACE FLIGHT↗
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Results for “SPACECREW”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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PSYCHOLOGICAL AND MEDICAL PROBLEMS IN SPACE FLIGHT
Magnitude and scope of the biomedical problems associated with placing a man in space
SPACECREW↗
DEVELOPMENT OF MANNED ARTIFICAL SATELLITES AND SPACE STATIONS
Survey of manned artificial satellites and space stations followed by operations and details of the x15, dynasoar, mercury and vostok
SPACECREW↗
United States Experience on the Utilization of Man's Capabilities in a Space Environment
Stresses on flight crew in space flight
SPACECREW↗
Minimum crew space habitability for the lunar mission
Psychological effects of restricted workspace and work-rest cycle on crew for lunar mission
PSYCHOLOGICAL EFFECT↗
Mission profiles
Sample mission profiles and planned scientific experiments for lunar landing crew
SPACECREW↗
Development of a flight-qualified whole-body dosimeter system Final report
Whole-body dosimeter system for monitoring radiation exposure to crew during space missions
RADIATION EXPOSURE↗
Astronaut selection and training.
Astronaut selection and crew preparation procedures for Gemini and Apollo programs
ASTRONAUT TRAINING↗
A model for the social system for the multiman extended duration space ship.
Model for social system for extended-duration spaceship crews subject to isolation, confinement and/or stress
GROUP BEHAVIOR↗
Gemini experiments program - Missions III - VII.
Gemini experiments program, examining crew integration, mission planning and prelaunch operations
SPACECREW↗
Lunar stay time extension module
Stay time extension module shelter structure to support 2 men for 8 days on lunar surface
SPACECREW↗
QADHD point-kernel radiation shielding computer code to evaluate propellant heating and dose to crew during engine operation
Point-kernel radiation shielding computer program to evaluate propellant heating and dose to crew during engine operation
RADIATION DOSE↗
A model for the social system for the multiman extended duration space ship.
Model for social system for extended-duration spaceship crews subject to isolation, confinement and/or stress
ASTRONAUT PERFORMANCE↗
Gemini experiments program - Mission III-VII.
Gemini experiments program, examining crew integration, mission planning and prelaunch operations
MISSION PLANNING↗
The Flexible Lunar Architecture for Exploration (FLARE): Designed for the Artemis-3 Moon 2024 Mission and Beyond
The Flexible Lunar Architecture for Exploration (FLARE) is a concept to deliver four crew to the lunar surface for 7 to 14 days and then return them safely to Earth by 2024. This meets NASA’s internal 2024 lunar landing deadline directed by President Trump (Trump, 2017) and the “5-year” goal set forth by Vice President Pence (Pence, 2019). FLARE is an alternative to NASA’s Human Landing System reference architecture from the Design Analysis Cycle (DAC) #2 (NASA, 2019b). The minimum FLARE concept uses one Space Launch System launch, one Orion, one European Service Module (ESM), and one human lander to deliver four crew to the Moon for a minimum surface duration of 7 days and return them to Earth. FLARE adds a new capability, called the SpaceTug, based upon the mature and successful United Launch Alliance “Common” Centaur Upper Stage vehicle, with modifications. In FLARE, the SpaceTug provides propulsion needed to return the Orion+ESM from the Moon to Earth. The SpaceTug also provides propulsion to deliver the human lander Descent Element (DE) and Ascent Element (AE) separately to lunar orbit. The Orion+ESM then completes a rendezvous with the mated DE+AE in lunar orbit. FLARE also offers optional phases to the Moon 2024 mission. The SpaceTug can also deliver components of the planned Gateway - including the Power and Propulsion Element and the Habitation and Logistics Outpost - to lunar orbit; however, the planned FLARE destination is a Low Lunar Frozen Polar Orbit unlike the NASA DAC2 plan for a Near Rectilinear Halo Orbit. FLARE also provides an option to deliver precursor equipment - including a habitation module, crew mobility devices and an In-Situ Resource Utilization demonstration - to the lunar surface for enhanced crew exploration and science with the extended 14-day surface mission.
Commercial Launch Vehicles (CLV)↗