"Launch Vehicle Recovery System Requirements."
The primary considerations in the design and development of a recovery system applicable to present expendable first stage launch vehicles are discussed. The general requirements that define the essential characteristics of a feasible recovery system are derived from three critical phases during fl...
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University of Alabama in Huntsville Archives
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| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10941 |
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Electronic |
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Saturn V Collection |
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University of Alabama in Huntsville Archives |
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University of Alabama in Huntsville Archives |
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Documents |
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Documents "Launch Vehicle Recovery System Requirements." Barraza, R. M. |
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Documents Saturn project Saturn launch vehicles Astronautics Recovery |
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The primary considerations in the design and development of a recovery system applicable to present expendable first stage launch vehicles are discussed. The general requirements that define the essential characteristics of a feasible recovery system are derived from three critical phases during flight. The degree of criticalness is primarily influenced by the conditions at stage cutoff and separation. The three critical phses of flight are broken down into the following: (1) conditions and requirements between stage separation to re-entry; (2) re-entry; and (3) terminal descent and landing. |
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"Launch Vehicle Recovery System Requirements."Barraza, R. M.Saturn projectSaturn launch vehiclesAstronauticsRecoveryThe primary considerations in the design and development of a recovery system applicable to present expendable first stage launch vehicles are discussed. The general requirements that define the essential characteristics of a feasible recovery system are derived from three critical phases during flight. The degree of criticalness is primarily influenced by the conditions at stage cutoff and separation. The three critical phses of flight are broken down into the following: (1) conditions and requirements between stage separation to re-entry; (2) re-entry; and (3) terminal descent and landing.1962-10-01TextDesign Analyseslaunvehirecosystrequ_061407154402.pdf TWO COPIESspc_stnv_000368http://libarchstor2.uah.edu/digitalcollections/items/show/10941http://libarchstor2.uah.edu/digitalcollections/files/original/20/10941/launvehirecosystrequ_061407154402.pdfSaturn V CollectionBox 7, Folder 30University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabamaenspc_stnv_000350_000374This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. |
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"Launch Vehicle Recovery System Requirements." |
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"Launch Vehicle Recovery System Requirements." |
| author |
Barraza, R. M. |
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Barraza, R. M. |
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UAHsaturnv10941 |
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http://libarchstor2.uah.edu/digitalcollections/items/show/10941 |
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1790443372064800768 |