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Aerobraking Characteristics For Several Potential Manned Mars Entry Vehicles
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Book Synopsis Aerobraking Characteristics for Several Potential Manned Mars Entry Vehicles by : Paul V. Tartabini
Download or read book Aerobraking Characteristics for Several Potential Manned Mars Entry Vehicles written by Paul V. Tartabini and published by . This book was released on 1989 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722052553 Total Pages :30 pages Book Rating :4.0/5 (525 download)
Book Synopsis Aerobraking Characteristics for Several Potential Manned Mars Entry Vehicles by : National Aeronautics and Space Administration (NASA)
Download or read book Aerobraking Characteristics for Several Potential Manned Mars Entry Vehicles written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-30 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: While a reduction in weight is always desirable for any space vehicle, it is crucial for vehicles to be used in the proposed Manned Mars Mission (MMM). One such way to reduce a spacecraft's weight is through aeroassist braking which is an alternative to retro-rockets, the traditional method of slowing a craft approaching from a high energy orbit. In this paper aeroassist braking was examined for two blunt vehicle configurations and one streamlined configuration. For each vehicle type, a range of lift-to-drag ratios was examined and the entry angle windows, bank profiles, and trajectory parameters were recorded here. In addition, the sensitivities of velocity and acceleration with respect to the entry angle and bank angles were included. Also, the effect of using different atmosphere models was tested by incorporating several models into the simulation program. Tartabini, Paul V. and Suit, William T. Langley Research Center RTOP 506-46-21-01...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722600365 Total Pages :32 pages Book Rating :4.6/5 (3 download)
Book Synopsis Preliminary Investigation of Parameter Sensitivities for Atmospheric Entry and Aerobraking at Mars by : National Aeronautics and Space Administration (NASA)
Download or read book Preliminary Investigation of Parameter Sensitivities for Atmospheric Entry and Aerobraking at Mars written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The proposed manned Mars mission will need to be as weight efficient as possible. A way of lowering the weight of the vehicle by using aeroassist braking instead of retro-rockets to slow a craft once it reaches its destination is discussed. The two vehicles studied are a small vehicle similar in size to the Mars Rover Sample Return (MRSR) vehicle and a larger vehicle similar in size to a six-person Manned Mars Mission (MMM) vehicle. Simulated entries were made using various coefficients of lift (C sub L), coefficients of drag (C sub D), and lift-to-drag ratios (L/D). A range of acceptable flight path angles with their corresponding bank angle profiles was found for each case studied. These ranges were then compared, and the results are reported here. The sensitivity of velocity and acceleration to changes in flight path angle and bank angle is also included to indicate potential problem areas for guidance and navigation system design. Lee, Mary C. and Suit, William T. Langley Research Center RTOP 506-46-21-01...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722807658 Total Pages :80 pages Book Rating :4.8/5 (76 download)
Book Synopsis The Effect of Interplanetary Trajectory Options on a Manned Mars Aerobrake Configuration by : National Aeronautics and Space Administration (NASA)
Download or read book The Effect of Interplanetary Trajectory Options on a Manned Mars Aerobrake Configuration written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-16 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: Manned Mars missions originating in low Earth orbit (LEO) in the time frame 2010 to 2025 were analyzed to identify preferred mission opportunities and their associated vehicle and trajectory characteristics. Interplanetary and Mars atmospheric trajectory options were examined under the constraints of an initial manned exploration scenario. Two chemically propelled vehicle options were considered: (1) an all propulsive configuration, and (2) a configuration which employs aerobraking at Earth and Mars with low lift/drag (L/D) shapes. Both the interplanetary trajectory options as well as the Mars atmospheric passage are addressed to provide a coupled trajectory simulation. Direct and Venus swingby interplanetary transfers with a 60 day Mars stopover are considered. The range and variation in both Earth and Mars entry velocity are also defined. Two promising mission strategies emerged from the study: (1) a 1.0 to 2.0 year Venus swingby mission, and (2) a 2.0 to 2.5 year direct mission. Through careful trajectory selection, 11 mission opportunities are identified in which the Mars entry velocity is between 6 and 10 km/sec and Earth entry velocity ranges from 11.5 to 12.5 km/sec. Simulation of the Earth return aerobraking maneuver is not performed. It is shown that a low L/D configuration is not feasible for Mars aerobraking without substantial improvements in the interplanetary navigation system. However, even with an advanced navigation system, entry corridor and aerothermal requirements restrict the number of potential mission opportunities. It is also shown that for a large blunt Mars aerobrake configuration, the effects of radiative heating can be significant at entry velocities as low as 6.2 km/sec and will grow to dominate the aerothermal environment at entry velocities above 8.5 km/sec. Despite the additional system complexity associated with an aerobraking vehicle, the use of aerobraking was shown to significantly lower the required initial LEO weight. In compari...
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 700 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Book Synopsis Monthly Catalog of United States Government Publications by :
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Book Synopsis Monthly Catalogue, United States Public Documents by :
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Book Synopsis Effect of Interplanetary Trajectory Options on a Manned Mars Aerobrake Configuration by : Robert D. Braun
Download or read book Effect of Interplanetary Trajectory Options on a Manned Mars Aerobrake Configuration written by Robert D. Braun and published by . This book was released on 1990 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index by :
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Book Synopsis International Exploration of Mars by :
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Book Synopsis NASA Technical Paper by : United States. National Aeronautics and Space Administration
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