Gemini 10 Launches Set for July 18
Preflight and flight activities of Gemini 10 launch - tracking, crew training, mission profile, and times of major events
SEARCH · Search NASA
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Preflight and flight activities of Gemini 10 launch - tracking, crew training, mission profile, and times of major events
The purpose of this paper is to review some of the more recent simulator results with emphasis on the airplane-design problem areas. Some of the simulator requirements for V/STOL and a low-altitude attack airplane will also be presented. Areas requiring additional effort are discussed briefly. Simulators for crew training however, are not considered in this paper.
Exospheric experimental test flights planning, crew training, flight-plan criteria and mission objectives
Real time interpretive simulation of lunar module digital autopilot program for flight crew training
Entry crew procedure information for use in flight planning, crew training, and preparing onboard data
Entry crew procedures information for use in flight planning, crew training, and preparing onboard data for C prime mission
Computer simulation and equations of motion for Apollo 8 crew training for lunar entries
Rendezvous procedures for LM-5 and CSM for use in crew training and flight planning
Rendezvous procedures for LM-4 and CSM for use in crew training and flight planning
Earth orbital space stations modular design, discussing space shuttle use, crew training and program management
Spacecraft development, mission design planning, flight crew operations, and flight operations are considered. Spacecraft design principles and test activities are described. Determination of the best series of flights leading to a lunar landing at the earliest possible time, flight planning, techniques for establishing flight procedures and carrying out flight operations, and crew training and simulation activities are discussed.
The tasks are defined required to design, develop produce, and field support a shuttle mission simulator for training crew members and ground support personnel. The requirements for program management, control, systems engineering, design and development are discussed along with the design and construction standards, software design, control and display, communication and tracking, and systems integration.
Articles pertaining to the solar studies and the Skylab program are presented, with emphasis on the usefulness of the Apollo Telescope Mount (ATM) program. A description of Skylab objectives and key mission events is included along with articles about the sun. Skylab solar studies which are reported include these topics: ATM solar observatory, scientific instruments, crew operations and crew training, and the joint observing program. The Skylab associated solar programs are also reported.
The Skylab Student Science Program was an effort on the part of NASA and the National Science Teachers Association (NSTA) to provide the youth of America an opportunity to directly participate in space research. Students across the nation submitted proposed experiments which were scientifically evaluated by the NSTA. From the more than three thousand experiments submitted, twenty-five of the most innovative and novel experiments were selected for flight. Many of these required the development of flight hardware in order to perform the experiments aboard Skylab. The requirements placed on the hardware in terms of cost, development time, weight, volume, and crew training represented a unique challenge to the NASA engineers and scientists involved in the design, development, fabrication and testing of this hardware. To meet these stringent requirements required innovative changes in the classic Skylab approach to experiment development.
A brief survey is made of significant aspects of the Skylab missions, with emphasis on atmospheric control, electrical power, stabilization and attitude control, prevention of instrument contamination, habitability of the spacecraft, in-flight maintenance and repair, and crew training. Skylab, unlike previous manned spacecraft, had a two-gas atmosphere of oxygen and nitrogen. The station's 25-kW capability was the largest electrical system ever flown in space. Skylab was the first flight application of large control-moment gyroscopes for attitude control. The missions provided significant scientific data in the fields of solar physics, biomedicine, earth resources, and materials processing. Particularly important was the finding of no physical limitation to men's ability to work in space for long periods.
A brief overview is presented of the Apollo-Soyuz Test Project. The mission objectives are summarized, and the mission profile is described. Other topics discussed include the reasons why the U.S. built the docking module, Soviet expenditures, use of the ATS-6 relay satellite to improve communications and television coverage, crew training, and safety aspects of the Soyuz spacecraft. It is noted that technology transfer has been minimal and that joint U.S.-Soviet space exploration may be a result of the project.
Extendible booms used to convey film cassettes weighing 56.7 kg (125 lb) between the Airlock Module and the Apollo Telescope Mount are described along with the dispensing mechanism. Problems encountered with the mechanism during the test program are discussed. These problems were mainly associated with operation in cold temperature, lubrication, and the motor/gearhead assembly. Another set of problems which arose during crew training in the MSFC water tank is also discussed.
Alternative approaches to payload operations planning and control and flight crew training are defined for spacelab payloads with the goal of: lowering FY77 and FY 78 costs for new starts; lowering costs to achieve Spacelab operational capability; and minimizing the cost per Spacelab flight. These alternatives attempt to minimize duplication of hardware, software, and personnel, and the investment in supporting facility and equipment. Of particular importance is the possible reduction of equipment, software, and manpower resources such as comtational systems, trainers, and simulators.