Design of spacecraft for manned planetary missions.
Spacecraft design for manned planetary landings noting mission characteristics, navigation requirements, crew housing, etc
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Spacecraft design for manned planetary landings noting mission characteristics, navigation requirements, crew housing, etc
As manned spacecraft have grown larger and more complex, they have come to rely on spacewalks or Extravehicular Activities (EVA) for both mission success and crew safety. Typically these spacecraft maintain all of the hardware and trained personnel needed to perform an EVA on-board at all times. Maintaining this capability requires volume and up-mass for storage of EVA hardware, crew time for ground and on-orbit training, and on-orbit maintenance of EVA hardware . This paper proposes an alternative methodology to utilize launch-on-need hardware and crew to provide EVA capability for space stations in Earth orbit after assembly complete, in the same way that most people would call a repairman to fix something at their home. This approach would not only reduce ground training requirements and save Intravehicular Activity (IVA) crew time in the form of EVA hardware maintenance and on-orbit training, but would also lead to more efficient EVAs because they would be performed by specialists with detailed knowledge and training stemming from their direct involvement in the development of the EVA. The on-orbit crew would then be available to focus on the immediate response to the failure as well as the day-to-day operations of the spacecraft and payloads. This paper will look at how current ISS unplanned EVAs are conducted, including the time required for preparation, and offer alternatives for future spacecraft utilizing lessons learned from ISS. As this methodology relies entirely on the on-time and on-need launch of spacecraft, any space station that utilized this approach would need a robust transportation system including more than one launch vehicle capable of carrying crew. In addition the fault tolerance of the space station would be an important consideration in how much time was available for EVA preparation after the failure. Each future program would have to weigh the risk of on-time launch against the increase in available crew time for the main objective of the spacecraft.
Apollo Manned Spacecraft Program systems design requirements, emphasizing instrumentation system and Phase I spacecraft
A general research program to explore the technical problem of rotating manned spacecraft has been underway at the Langley Research Center for some time. A report summarizing progress on some of the more significant aspects of the work accomplished thus far was recently presented to a group of NASA personnel sharing interest in this work at a symposium held at the Langley Research Center from July 31 to August 1, 1962. The collection of papers contained in this report is a summary of the material presented. It is published in this form for the convenience of other organizations and individuals who may engaged in similar studies. It is emphasized that the investigations reported herein are exploratory in nature. There is no approved NASA program for the construction and operation of any such spacecraft.
Sensitivity of manned planetary spacecraft design to shield weight, onboard radiation and uncertainties in space environment radiation
Navigation and guidance analysis of Mars probe launched from manned flyby spacecraft for 1975- 1976
Trajectory optimization for Mars and Venus flights by manned spacecraft
Deduction of reentry near wake plasma properties for Mercury and Gemini manned orbital spacecraft from radio signal attenuation data
Navigation and guidance analysis of Mars probe launched from manned flyby spacecraft
The historic earth orbital flight of the Mercury space capsule on February 20, 1962 has illustrated that man has the capability of creating instrumentation and equipment which permit him to survive outside the protective earth atmosphere which, in time, has served both as a shield and a barrier. Because of this great achievement man need no longer restrict himself to earth-space but may direct his resources to expand his zone of operation to earth-moon space. However, in order to exploit this new frontier many problems must be solved which are not mere extensions or extrapolations of those already treated. The problem associated with providing man with an adequate environment for extended periods in the earth's atmosphere, earth-moon space and on the lunar surface is indeed extensive. Trapped radiation, solar flare activity, meteoroid bombardment, solar radiation and the hard vacuum of space are no longer merely phenomena. of scientific interest; they describe the operating environment of manned earth-lunar spacecraft. In order that man may effectively operate in the earth-moon space, myriads of systems and subsystems of varying types and functions must be devised and integrated into an efficient, reliable man-machine complex. This paper will consider only one small aspect of this problem--that is, the problem of providing man with an adequate gaseous and thermal environment in earth-lunar spacecraft. Control of atmospheric gases in manned sealed environments will be treated in Part I. Part II treats thermal regulation and atmosphere control requirements of mobile life support systems for lunar exploration.
Preliminary study of spacecraft design factors for manned mars orbiting and landing missions
Ten former NASA astronauts were interviewed using a set of 51 questions developed to encourage the contacts to discuss any thoughts, opinions, conclusions, or suggestions which might have evolved since they left the astronaut program. Strict confidentiality was maintained. At least one astronaut from each of the NASA manned space flight programs, excluding the Space Transportation System (Shuttle), was interviewed. The report records the answers to the questions asked, spontaneous comments, and the investigator's own personal evaluations of the material obtained. No statistical analysis of the material was attempted. The professional opinions of these ten experienced astronauts will be of value to persons concerned with the design and operation of manned spacecraft and manned space stations.
Spacecraft, space acceleration system, and earth based support for integrated manned, interplanetary spacecraft concepts
Subsystem design criteria for integrated manned interplanetary spacecraft concept
Hand-held hygrometer for measuring dew point and surface temperature inside Gemini manned spacecraft
Problems in developing aircraft and spacecraft manned flight research simulation facilities