3 edition of A two-stage-to-orbit spaceplane concept with growth potential found in the catalog.
A two-stage-to-orbit spaceplane concept with growth potential
Unmeel B. Mehta
by National Aeronautics and Space Administration, Ames Research Center, Available from NASA Center for AeroSpace Information in Moffett Field, Calif, Hanover, MD
Written in English
|Other titles||Two stage to orbit spaceplane concept with growth potential.|
|Statement||Unmeel B. Mehta, Jeffrey V. Bowles.|
|Series||[NASA technical memorandum] -- NASA/TM-2001-209620., NASA technical memorandum -- 209620.|
|Contributions||Bowles, Jeffrey V., Ames Research Center.|
|The Physical Object|
Champions of the reusable concept assert that the lowest cost approach (they claim in fact, "the only way to achieve truly low cost") is to develop a highly reusable (up to 50 or 60 missions before overhaul), preferably single stage to orbit, vehicle that can be turned around for re-flight. Abstract - This paper describes a qualitative business plan for starting a space tourism business. The first step is the development of the Ascender small sub-orbital spaceplane - a sort of "re-invented X" - designed for quick turnaround, and capable of carrying two pilots and either experiments or two passengers. Ascender uses no new technology and could be flying in three years.
Blackstar: The two-stage-to-orbit Spaceplane. During the s, Soviet-era aerospace companies developed plans for what they called a “space fighter.” The primary roles for this spaceplane concept were the following: military reconnaissance, satellite interception, space station defense, and crew transfer applications. The Intermediate eXperimental Vehicle (IXV) is a European Space Agency (ESA) experimental suborbital re-entry vehicle. It was developed to serve as a prototype spaceplane to validate the ESA's work in the field of reusable launchers. Intermediate eXperimental Vehicle - WikiMili, The Free Encyclopedi.
Early two-stage-to-orbit shuttle study, using storable propellants, Dynasoar-configuration delta wing orbiter and booster. RBSS American winged orbital launch vehicle. The Recoverable Booster Space System was a plan circulated in the early 's to use the XB as a recoverable supersonic first stage for a range of systems. Falcon 9 is a two-stage-to-orbit medium lift launch vehicle designed and manufactured by SpaceX in the United States. It is powered by Merlin engines, also developed by SpaceX, burning liquid oxygen (LOX) and rocket-grade kerosene (RP-1) propellants. Its name is derived from the Millennium Falcon and the nine engines of the rocket's first stage. The rocket evolved with versions v (
Student questionnaire and test results by academic ability, socioeconomic status, and region
50 egg recipes
Phénoménologie de la mort
Mosquitoes of the Ethiopian region ...
A Window on My World
Education for Uncertainty H (No Series Description Provided)
Tables of bolometric luminosity functions
Local management of colleges
Davenport Bros. & Co.
Multivariate Statistical Analysis in Geography
Doctor in the house
William James and other essays on the philosophy of life
man with the hoe
A Two-Stage-to-Orbit Spaceplane Concept With Growth Potential [Mehta, Unmeel B., Bowles, Jeffrey V., NASA Technical Reports Server (NTRS)] on *FREE* shipping on qualifying offers.
A Two-Stage-to-Orbit Spaceplane Concept With Growth PotentialCited by: A TWO-STAGE-TO-ORBIT SPACEPLANE CONCEPT WITH GROWTH POTENTIAL Unmeel B. Mehta and Jeffrey V. Bowles NASA Ames Research Center, Moffett Field, California, U.S.A.
Abstract A two-stage-to-orbit (TSTO) spaceplane concept developed in is revisited, and new information is provided to assist in the development of the next-File Size: 1MB. Full text of "A Two-Stage-to-Orbit Spaceplane Concept With Growth Potential" See other formats NASA/TM A Two-Stage-to-Orbit Spaceplane Concept with Growth Potential Unmeel B.
Mehta and Jeffrey V. Bowles February The NASA STI Program Office in Profile Since its founding, NASA has been dedicated to the advancement of aeronautics and space science.
A Two-Stage-to-Orbit Spaceplane Concept With Growth Potential Article in Journal of Propulsion and Power 17(6) March with 52 Reads How we measure 'reads'. Two-stage-to-orbit spaceplane concept with growth potential (OCoLC) Material Type: Government publication, National government publication, Internet resource: Document Type: Book, Internet Resource: All Authors / Contributors: Unmeel B Mehta; Jeffrey V.
Two-stage-to-orbit spaceplane concept with growth potential (OCoLC) Material Type: Document, Government publication, National government publication, Internet resource: Document Type: Internet Resource, Computer File: All Authors / Contributors: Unmeel B Mehta; Jeffrey V Bowles; Ames Research Center.
A two-stage-to-orbit (TSTO) spaceplane concept developed in is revisited, and new information is provided to assist in the development of the next-generation space transportation vehicles. The design philosophy, TSTO spaceplane concept, and the design method are briefly described.
A spaceplane is an aerospace vehicle that can fly/glide like an aircraft in Earth's atmosphere and maneuver like a spacecraft in the vacuum of space. To do so, spaceplanes must incorporate features of both aircraft and spacecraft, occupying an intermediate space between the two. Orbital spaceplanes are more like spacecraft, while sub-orbital spaceplanes are more like fixed-wing aircraft.
This classic history of America's high-stakes quest to dominate the skies is "a gripping technothriller in which the technology is real" (New York Times Book Review). From the development of the U-2 to the Stealth fighter, Skunk Works is the true story of America's most secret and.
A Two-Stage-To-Orbit Spaceplane Concept with Growth Potential. Unmeel B Mehta. 06 Aug Paperback. US$ SKUNK-WORKS-A-PERSONAL-MEMOIR-OF-MY-YEARS-AT-LOCKHEED Click Download or Read Online button to SKUNK-WORKS-A-PERSONAL-MEMOIR-OF-MY-YEARS-AT-LOCKHEED book pdf for free now.
Skunk Works. Author: Ben R. Rich ISBN: Genre: History File Size: MB A Two Stage To Orbit Spaceplane Concept With Growth Potential. Author. A two-stage-to-orbit (TSTO) or two-stage rocket launch vehicle is a spacecraft in which two distinct stages provide propulsion consecutively in order to achieve orbital velocity.
It is intermediate between a three-stage-to-orbit launcher and a hypothetical single-stage-to-orbit (SSTO) launcher. At liftoff the first stage is responsible for accelerating the vehicle. 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference.
Two SABREs will power Skylon — a privately funded, single-stage-to-orbit concept vehicle that is feet (84 meters) long. At takeoff, the plane will weigh about tons (, kilograms). A single-stage-to-orbit (or SSTO) vehicle reaches orbit from the surface of a body using only propellants and fluids and without expending tanks, engines, or other major hardware.
The term usually, but not exclusively, refers to reusable vehicles. No Earth-launched SSTO launch vehicles have ever been constructed. To date, orbital launches from Earth have been performed by either fully or.
A two-stage-to-orbit (TSTO) spaceplane concept developed in is revisited, and new information is provided to assist in the development of the next-generation space transportation vehicles.
U.S. and European aerospace companies have pushed two-stage-to-orbit (TSTO) spaceplane concepts for decades. Most large U.S. airframe manufacturers designed spaceplane-type vehicles during the s and '60s, and XB program documents include a concept for carrying and launching a low-Earth orbiter.
There is an Open Access version for this licensed article that can be read free of charge and without license restrictions.
The content of the Open Access version may differ from that of the licensed version. The Defense Advanced Research Projects Agency (DARPA) is looking to develop a fully-reusable unmanned spaceplane, and they are now ready to start working their proposed Experimental Spaceplane (XS-1).
The next proposal was for a spaceplane similar in concept to the US Space Shuttle but a little more advanced. Dubbed V-2, it was suggested by a third division of the Ministry of Aerospace Industry.
Like Changcheng 1 this was a two-stage vertical takeoff system, the difference with the first stage being that it was recoverable like that of the. The simplest of the four approaches suggested was Tianjiao 1 (“First in Space 1”), jointly proposed by the Shanghai Academy of Spaceflight Technology (SAST—the later developer of the Shenzhou capsule) and the aircraft division of the Ministry of Aerospace Industry.
This was virtually an exact copy of the American shuttle or Buran’s aerodynamic shape, with only upturned wingtips, but a.WoodenKnight writes "India's ISRO Chairman, G Madhavan Nair recently gave a brief description of a fully-reusable 2-stage satellite launch vehicle that is being planned at ISRO.
From the article: 'This is in its initial stages of vehicle configuration and the first stage is configured as a winged bo.TSTO spaceplanes: by IKE - Boeing (SSME) This part of the present article is based on a patent application filed by Boeing in (US 4,). This system is described in two variations, the one with an orbital vehicle that uses a liquid fuel rocket engine and the other with an orbiter using a scramjet.
The carrier mothership is.