Sensitivity of long-duration manned spacecraft design to environmental uncertainties.
Long duration manned spacecraft design sensitivity to environmental uncertainties
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Long duration manned spacecraft design sensitivity to environmental uncertainties
Aerothermodynamic phenomena associated with reentry of manned spacecraft
Microorganism growth control in manned spacecraft environment
An analysis, in terms of key design parameters, is presented of a digital link for bidirectional communication between an advanced manned spacecraft, such as the space shuttle, and a ground terminal by means of a synchronous communication relay satellite. Performance of both ground to manned spacecraft and return links are compared with and without coding. A breadboard terminal for simulating the two-way link is described. Results of error rate tests are discussed.
Description of test facilities used to develop manned spacecraft
Oxygen reclamation system with electrolysis cell for reduction of carbon dioxide on manned spacecraft
Night airglow photographed from Gemini series of manned spacecraft, noting consistency with rocket and Mercury spacecraft measurements
Reliability of electrical power subsystem designed for manned spacecraft
Carbon dioxide removal and control methods for manned spacecraft cabin atmospheres, comparing Molecular Sieve regenerative sorber and LiOH nonregenerative systems
Cost estimate model for manned spacecraft systems
The overall management approach to the NASA Phase B definition studies for space stations, which were initiated in September 1969 and completed in July 1972, is reviewed with particular emphasis placed on the management approach used by the Manned Spacecraft Center. The internal working organizations of the Manned Spacecraft Center and its prime contractor, North American Rockwell, are delineated along with the interfacing techniques used for the joint Government and industry study. Working interfaces with other NASA centers, industry, and Government agencies are briefly highlighted. The controlling documentation for the study (such as guidelines and constraints, bibliography, and key personnel) is reviewed. The historical background and content of the experiment program prepared for use in this Phase B study are outlined and management concepts that may be considered for future programs are proposed.
Advanced manned spacecraft heat shield thermal strain analysis - equilibrium and stress equations, singular point, and computer program
Attitude stabilization of manned spacecraft by twin gyros and pulse-modulated reaction jets
Compressed digital television system design for transmitting information from manned spacecraft
The Saffire Experiment represents the first test of spacecraft fires at a scale relevant to real spacecraft. Although large-scale fire tests on Earth are conducted for every type of habitable structure (buildings, planes, trains, automobiles, ships and mines) they had never been attempted in a space experiment for obvious reasons of practicality and safety. This is despite the fact that fire is a catastrophic hazard for spaceflight where the crew has very limited or no escape options. The spread and growth of a fire, combined with its interactions with the vehicle cannot be expected to scale linearly from small-scale test data, and so there is a substantial gap in our ability to predict the behavior of spacecraft fire and also its impact on the spacecraft habitability and operability. The experiments were performed aboard the Cygnus vehicle, a large unmanned resupply spacecraft to the International Space Station (ISS). The experiment was installed in the Cygnus vehicle, and remained dormant during docked operations. Once the vehicle was reloaded with ISS trash, it unberthed and moved to a separate orbit. The Saffire experiment was initiated by ground command and downlinked the data before the vehicle re-entered into the earth's atmosphere. The downloaded test data show resolved the question of whether flame growth will achieve a steady size and demonstrated that the size of the enclosure surrounding the sample has more impact on the flame spread than anticipated.
Graphical cost estimating procedure for advanced manned spacecraft
Heatless adsorption techniques for carbon dioxide removal in manned spacecraft
Heatless desorption technology for carbon dioxide control in manned spacecraft