4 edition of Orbiter rarefied-flow reentry measurements from the OARE on STS-62 found in the catalog.
Orbiter rarefied-flow reentry measurements from the OARE on STS-62
Published
1995
by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va
.
Written in
Edition Notes
Other titles | Orbiter rarefied flow reentry measurements from the OARE on STS-62. |
Statement | R.C. Blanchard, J.Y. Nicholson. |
Series | NASA technical memorandum -- 110182. |
Contributions | Nicholson, J. Y., Langley Research Center. |
The Physical Object | |
---|---|
Format | Microform |
Pagination | 1 v. |
ID Numbers | |
Open Library | OL17791965M |
OCLC/WorldCa | 34072054 |
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Orbiter Rarefied-Flow Reentry Measurements from the OARE on STS Robert C. Blanchard NASA Langley Research Center Hampton, Virginia John Y. Nicholson ViGYAN, Inc. Hampton, Virginia Abstract Acceleration data taken from the Orbital Acceleration Research Experiment (OARE) during reentry on STS has been analyzed using.
To date, the Orbital Acceleration Research Experiment (OARE) has flown on the shuttle orbiter for five missions; namely, STS, STS, STS, STS, and STS Acceleration data taken from the Orbital Acceleration Research Experiment (OARE) during reentry on STS has been analyzed using calibration factors taken on-orbit.
The data includes the flight regime from orbital altitudes down to about km which covers the free-molecule-flow regime and some of the flow-transition into the hypersonic by: 5. Add tags for "Orbiter rarefied-flow reentry measurements from the OARE on STS".
Be the first. Acceleration data taken from the Orbital Acceleration Research Experiment (OARE) during reentry on STS has been analyzed using calibration factors taken on-orbit. The data examined include the flight regime from orbital altitudes down to about km which covers the free-moleculeflow regime and the upper altitude fringes of the flow-transition into the hypersonic : Robert C.
Blanchard and John Y. Nicholson. Acceleration data taken from the Orbital Acceleration Research Experiment (OARE) during reentry on STS has been analyzed using calibration factors taken on-orbit.
Orbiter rarefied-flow reentry measurements from the OARE on STS Space acceleration measurement system description and operations on the First Spacelab Life Sciences Mission.
Spacelab Life Sciences STS Press Kit. Media Resouce Kit. Mission Safety Evaluation Report. Debris/ice/TPS assessment and photographic analysis for Shuttle. Acceleration data taken from the Orbital Acceleration Research Experiment (OARE) during reentry on STS have been analyzed using calibration factors taken on orbit.
Yes and no. While I don't make alignment burns, this tutorial is designed for beginners (hence the "for Dummies"). The base alignment allows the re-entry to be viewed as a two dimensional problem (Altitude and distance) rather than a three dimensional problem.
Once one has mastered the two dimensional re-entry, the third dimension is easy to add. This is the first Orbiter mission which collected OARE data during the Orbiter reentry phase. The data examined include the flight regime from orbital altitudes down to about 90 km which covers the free-molecule-flow regime and the upper altitude fringes of the.
Blanchard and J. Nicholson, Orbiter Rarefied-Flow Reentry Measurements From the OARE on STS, NASA TM, Junepp. 35, Only pages of the report are viewable. (MB). Signi cant discoveries about gas–surface interactions that have been made in 90 years of laboratory experiments and 30 years of orbital measurements are reviewed.
This information is used to improve the calculation of drag coef cients for satellites in low Earth orbit for several different satellite shapes and orientations by inserting the appropriate parameters in theoretical models of the. Sling Rental. Service & Warranty.
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Started by damascus. 3 Replies Views 16 Augustby Hawxx: New Orbiter Started by darkvoid. 15 Replies Views. Consider the spacecraft depicted schematically in Fig. 3, where the random vector pressure field, Z (x; t), models the loading during atmospheric re-entry, where x and t denote location on the outer surface of the spacecraft and time, respectively.
The spacecraft, shown here as a perfect cone, has several stiffening ribs oriented in the hoop direction; a base ring is located at the aft end of Cited by: STS was a Space Shuttle program mission flown aboard Space Shuttle primary payloads were the USMP microgravity experiments package and the OAST-2 engineering and technology payload, both in the orbiter's cargo or: NASA.
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During re-entry. The computed drag coefficients of compact satellites have a large dependence on altitude because the speed ratio decreases with increasing altitude, while the decreasing surface coverage causes the accommodation coefficients to coefficients also have a small dependence on time in the sunspot cycle (Moe et al., ) through the temperature and mean molecular by: ORBITER™ ST Steerable Catheter Ergonomically designed pole steerable catheter.
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ACCELEROMETER DATA ANALYSIS AND PRESENTATION TECHNIQUES | Acronym List accel a cc a gg a ggnew a ggOARE a new a OARE a, rouiew rotOARE avg CG cumRMS dF dT f f c fhigh Mow f N f s ftp g ORMS Hz J k L LSLE m M N acceleration vector magnitude acceleration at the Orbiter center of gravity, mapped from OARE acceleration due to gravity gradient.One way to accelerate orbital decay is to lower the perigee altitude so that atmospheric drag will cause the spacecraft to enter the Earth’s atmosphere more rapidly.
However, in.Orbiter rarefied-flow reentry measurements from the OARE on STS Space acceleration measurement system description and operations on the First Spacelab Life Sciences Mission. Spacelab Life Sciences STS Press Kit.
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