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Space Shuttle Orbiter Crew Hatch Jettison Test Using A 00405 Scale Model 16 0 In The Texas A M Low Speed Wind Tunnel Oa362 Space Shuttle Aerothermodynamic Data Report
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722789084 Total Pages :40 pages Book Rating :4.7/5 (89 download)
Book Synopsis Space Shuttle Orbiter Crew Hatch Jettison Test Using a 0.0405-Scale Model (16-0) in the Texas A/M Low Speed Wind Tunnel (Oa362). Space Shuttle Aerothermodynamic Data Report by : National Aeronautics and Space Administration (NASA)
Download or read book Space Shuttle Orbiter Crew Hatch Jettison Test Using a 0.0405-Scale Model (16-0) in the Texas A/M Low Speed Wind Tunnel (Oa362). Space Shuttle Aerothermodynamic Data Report written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-11 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains post-test information for the Space Shuttle Orbiter Crew Hatch Jettison Test OA362 which was conducted in the Texas A&M Low Speed Wind Tunnel from 6/15/87 to 6/22/87. The test objective was to verify that the crew hatch, once jettisoned, would clear the orbiter under various simulated flight conditions. Several model hatches were used with the 0.0405-scale orbiter (Model 16-0). The model's angle of attack was set at 10, 15, and 20 degrees while the sideslip had values of minus 5, 0, and plus 5 degrees. The full scale Qbars that were simulated were 105, 128, 160, and 210 psf. In the hatch jettison mechanism itself, the plunger pressure was varied to achieve horizontal velocities of 3, 5, 7, and 20.1 feet per second model scale, and the plunger location was varied to achieve a variety of rotational velocities. The orbiter model was subjected to 122 runs with 13 different hatches. Of these, 60 were good runs. Mitchell, C. E. Unspecified Center NAS9-17840...
Book Synopsis Space shuttle wind tunnel testing program summary by : A. M. Whitnah
Download or read book Space shuttle wind tunnel testing program summary written by A. M. Whitnah and published by . This book was released on 1985 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Shuttle Phase B Wind Tunnel Test Database by : J. L. Glynn
Download or read book Space Shuttle Phase B Wind Tunnel Test Database written by J. L. Glynn and published by . This book was released on 1988 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Grumman H-33 Space Shuttle Orbiter Aerodynamic and Handling-qualities Study by :
Download or read book Grumman H-33 Space Shuttle Orbiter Aerodynamic and Handling-qualities Study written by and published by . This book was released on 1972 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of a representative delta-wing orbiter, the Grumman H-33, that utilized external-hydrogen tanks has been completed. The study encompassed a detailed wind-tunnel program from subsonic to hypersonic speeds, analyses of the data, and the calculation and assessment of the orbiter handling qualities using the most aft center-of-gravity locations anticipated during entry and approach.
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781730879685 Total Pages :64 pages Book Rating :4.8/5 (796 download)
Book Synopsis Sts-78 Space Shuttle Mission Report by : National Aeronautics and Space Adm Nasa
Download or read book Sts-78 Space Shuttle Mission Report written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-06 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: The STS-78 Space Shuttle Program Mission Report summarizes the Payload activities as well as the Orbiter, External Tank (ET), Solid Rocket Booster (SRB), Reusable Solid Rocket Motor (RSRM), and the Space Shuttle main engine (SSME) systems performance during the seventy-eighth flight of the Space Shuttle Program, the fifty-third flight since the return-to-flight, and the twentieth flight of the Orbiter Columbia (OV-102). In addition to the Orbiter, the flight vehicle consisted of an ET that was designated ET-79; three SSME's that were designated as serial numbers 2041, 2039, and 2036 in positions 1, 2, and 3, respectively; and two SRB's that were designated BI-081. The RSRM's, designated RSRM-55, were installed in each SRB and the individual RSRM's were designated as 360L055A for the left SRB, and 360L055B for the right SRB. The STS-78 Space Shuttle Program Mission Report fulfills the Space Shuttle Program requirement as documented in NSTS 07700, Volume 7, Appendix E. The requirement stated in that document is that each organizational element supporting the Program will report the results of their hardware (and software) evaluation and mission performance plus identify all related in-flight anomalies. The primary objective of this flight was to successfully perform the planned operations of the Life and Microgravity Spacelab experiments. The secondary objectives of this flight were to complete the operations of the Orbital Acceleration Research Experiment (OARE), Biological Research in Canister Unit-Block II (BRIC), and the Shuttle Amateur Radio Experiment II-Configuration C (SAREX-II). The STS-78 mission was planned as a 16-day, plus one day flight plus two contingency days, which were available for weather avoidance or Orbiter contingency operations. The sequence of events for the STS-78 mission is shown in Table 1, and the Space Shuttle Vehicle Management Office Problem Tracking List is shown in Table 2. The Government Furnished Equipment/Flight Crew Equipment (GF...
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781793951847 Total Pages :34 pages Book Rating :4.9/5 (518 download)
Book Synopsis Turbulent Wing-Leading-Edge Correlation Assessment for the Shuttle Orbiter by : National Aeronautics and Space Adm Nasa
Download or read book Turbulent Wing-Leading-Edge Correlation Assessment for the Shuttle Orbiter written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2019-01-13 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study was conducted in support of the Orbiter damage assessment activity that takes place for each Shuttle mission since STS-107 (STS - Space Transportation System). As part of the damage assessment activity, the state of boundary layer (laminar or turbulent) during reentry needs to be estimated in order to define the aerothermal environment on the Orbiter. Premature turbulence on the wing leading edge (WLE) is possible if a surface irregularity promotes early transition and the resulting turbulent wedge flow contaminates the WLE flow. The objective of this analysis is to develop a criterion to determine if and when the flow along the WLE experiences turbulent heating given an incoming turbulent boundary layer that contaminates the attachment line. The data to be analyzed were all obtained as part of the MH-13 Space Shuttle Orbiter Aerothermodynamic Test conducted on a 1.8%-scale Orbiter model at Calspan/University of Buffalo Research Center in the Large Energy National Shock Tunnels facility. A rational framework was used to develop a means to assess the state of the WLE flow on the Orbiter during reentry given a contaminated attachment-line flow. Evidence of turbulent flow on the WLE has been recently documented for a few STS missions during the Orbiter s flight history, albeit late in the reentry trajectory. The criterion developed herein will be compared to these flight results. King, Rudolph A. and Vaughan, Matthew P. Langley Research Center NASA/TM-2009-215949, L-19784, LF99-9713
Book Synopsis Study of Several Factors Affecting Crew Escape Trajectories from the Space Shuttle Orbiter at Low-subsonic Speeds by :
Download or read book Study of Several Factors Affecting Crew Escape Trajectories from the Space Shuttle Orbiter at Low-subsonic Speeds written by and published by . This book was released on 1985 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
