词条 | Lockheed L-301 | |||||||||||||||||
释义 |
DevelopmentThe L-301 HGV was intended to be a follow-on to the X-15 and X-24 (specifically the X-24B) programs, to take lessons learned from both and integrate them into an airframe capable of at least reaching Mach 8 and engaging in hypersonic skip-glide maneuvers for long range missions. While the NASA program, one of several to use the tentative X-24C designator, was ostensibly canceled in 1977, it was only canceled at the time because of USAF disclosures of duplicate black programs with the same contractors for similar vehicles{{cn|date=December 2018}}. The vehicle used both air breathing ram or scramjet propulsion as well as a rocket engine, carrying both RP-1 and LH2 propellant as well as on-board stores of LOX. Drawings and mission profiles are available from the NASA website [4]. DesignPropulsionOriginally intended to carry the same XLR-99 engine used by the X-15, the primary engine was changed to the LR-105, which was the sustainer engine used on the Atlas launcher. This rocket engine, burning RP-1 and LOX, was intended to accelerate the X-24C to hypersonic speeds in order to ignite the hydrogen fueled, air breathing ram/scramjet mounted in the belly of the airframe with which it would attain cruise speeds of at least Mach 6 and peak velocities of Mach 8+ at altitudes of 90,000 feet or more. As such, this vehicle was plainly not intended to reach orbit. AirframeDesign of the aircraft in various wind tunnel models and contractor drawings seems to follow variations of the FDL-5 and FDL-8 lifting body shapes originally developed by the USAF Flight Dynamics Laboratory in the 1950s, which were used in the earlier X-23 and X-24A/B programs. With a radically swept delta wing, and 2, 3, or 4 vertical stabilizers, as well as several body flaps (depending on the model), the vehicle did not lack for control surfaces. The vehicle measured 74 feet 10 inches long, 24 ft, 2 in wingspan, and 20 ft, 7 in height. Various drawings show a payload bay twelve feet long and perhaps five feet diameter.[5] References1. ^1 https://books.google.com/books?id=DUkl5bH6k6EC&pg=PA98&lpg=PA98&dq=National+Hypersonic+Research+Facility+x-15+x-24c&source=bl&ots=Ubvm4kazo1&sig=16Y5rv1y8HLZX8fy8mHZGmDBev4&hl=en&ei=7exrSujtNpLWM4a5tPkG&sa=X&oi=book_result&ct=result&resnum=3 [Lockheed Secret Projects by Dennis R. Jenkins] 2. ^{{cite web |url=http://www.darpa.mil/tto/solicit/BAA08-53/VULCAN_Industry_Day_Presentations.pdf |title=Archived copy |accessdate=2009-07-26 |deadurl=yes |archiveurl=https://web.archive.org/web/20090725111504/http://www.darpa.mil/tto/solicit/BAA08-53/VULCAN_Industry_Day_Presentations.pdf |archivedate=2009-07-25 |df= }} ["X-24C NHRF"] 3. ^https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19790008668_1979008668.pdf [CONFIGURATION DEVELOPMENT STUDY OF THE X-24C HYPERSONIC RESEARCH AIRPLANE - PHASE II] 4. ^https://crgis.ndc.nasa.gov/crgis/images/5/54/PEN00250.pdf 5. ^https://crgis.ndc.nasa.gov/crgis/images/5/5d/PEN00272.pdf Further reading
External links
10 : Cancelled military aircraft projects of the United States|Lifting bodies|Lockheed aircraft|Crewed spacecraft|Hypersonic aircraft|Parasite aircraft|Rocket-powered aircraft|Scramjet-powered aircraft|Spaceplanes|Cancelled spacecraft |
|||||||||||||||||
随便看 |
|
开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。