Download or read book Systems Analysis of a Future Semi reusable Launcher Based on a High Thrust Bleed Cycle Rocket Engine written by A. Herbertz and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book 37th AIAA ASME SAE ASEE Joint Propulsion Conference Exhibit written by and published by . This book was released on 2001 with total page 522 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerospace America written by and published by . This book was released on 2001 with total page 720 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A New Rocket Based Combined Cycle for Reusable Launch Vehicles written by and published by . This book was released on 2000 with total page 85 pages. Available in PDF, EPUB and Kindle. Book excerpt: MSE Technology Applications, Inc., in cooperation with United Technologies Research Center and HyperTech Concepts Company, proposes to develop combined propulsion technology for a small reusable launch vehicle (RLV) known as the KLIN Cycle, which consists of a thermally integrated deeply cooled turbojet and a liquid rocket engine. The objective of this concept is to achieve a high pressure ratio in a simple, lightweight turbojet engine. The proven result is an exceptional engine thrust to weight ratio, as well as improved lsp and mass fraction of the launcher. For a heavy launcher, the KLIN Cycle promises RLV gross takeoff weight reduction by a factor of two with additional prospects of lower dry weight. When based on the RL10 engine family, the KLIN Cycle makes a small single stage to orbit and two stage to orbit RLV feasible and very economically attractive. The benefit of the KLIN Cycle to the U.S. Air Force is a low life cycle cost combined propulsion system for a space plane that can double existing rocket propulsion capabilities by the year 2010. The details of this proposed technology are presented in the report.

Download or read book Analysis of the Staging Maneuver and Booster Glideback Guidance for a Two stage Winged Fully Reusable Launch Vehicle written by J. Christopher Naftel and published by . This book was released on 1993 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Damage mitigating Control of a Reusable Rocket Engine for High Performance and Extended Life written by Asok Ray and published by . This book was released on 1995 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Reusable Launch System written by Fouad Sabry and published by One Billion Knowledgeable. This book was released on 2022-08-03 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt: What Is Reusable Launch System When transporting payloads from Earth's surface into outer space, a reusable launch vehicle has pieces that may be retrieved and used again in subsequent launches. The stages of the rocket are the most frequent component of the launch vehicle that is intended for reuse. There is also the possibility of reusing smaller components, like as rocket engines and boosters, however it is possible for reusable spacecraft to be launched atop an expendable launch vehicle. The production of these components is not required for reusable launch vehicles, which results in a considerable reduction in the overall cost of the launch. The expense of recovery and restoration, on the other hand, will reduce the value of these advantages. How You Will Benefit (I) Insights, and validations about the following topics: Chapter 1: Reusable launch system Chapter 2: Space Shuttle Chapter 3: Single-stage-to-orbit Chapter 4: Spacecraft Chapter 5: Space Shuttle program Chapter 6: Human spaceflight programs Chapter 7: Booster (rocketry) Chapter 8: Spaceplane Chapter 9: Space vehicle Chapter 10: Boeing X-37 Chapter 11: Dream Chaser Chapter 12: Launch vehicle Chapter 13: List of crewed spacecraft Chapter 14: Falcon 9 Chapter 15: Buran (spacecraft) Chapter 16: VTVL Chapter 17: Falcon Heavy Chapter 18: Takeoff and landing Chapter 19: SpaceX reusable launch system development program Chapter 20: XS-1 (spacecraft) Chapter 21: Super heavy-lift launch vehicle (II) Answering the public top questions about reusable launch system. (III) Real world examples for the usage of reusable launch system in many fields. (IV) 17 appendices to explain, briefly, 266 emerging technologies in each industry to have 360-degree full understanding of reusable launch system' technologies. Who This Book Is For Professionals, undergraduate and graduate students, enthusiasts, hobbyists, and those who want to go beyond basic knowledge or information for any kind of reusable launch system.

Download or read book Comparative System Analysis of Reusable Rocket and Air breathing Launch Vehicles written by Adam F. Dissel and published by . This book was released on 2005 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Describing function Analysis of the Stability of a Launch Vehicle with Nonlinear Thrust Vectoring written by Harold C. Lester and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Reusable Rocket Engine Intelligent Control System Framework Design Phase 2 written by and published by . This book was released on 1991 with total page 384 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Studies on Expander Bleed Cycle Engines for Launchers written by Martin Sippel and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Feasibility of SCRAMJET Technology for an Intermediate Propulsive Stage of an Expendable Launch Vehicle written by Michael D. Schafer and published by . This book was released on 2002 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: The single largest contributor to the cost of pulling objects into space is that of the launch portion. The currently available chemical rockets are only capable of specific impulse (Isp) values on the average of 300-350 seconds, with a maximum of 450 seconds. In order to improve the performance of the current families of launch vehicles, it is necessary to increase the performance of the rocket motors, and conversely the amount of propellant/ oxidizer carried. The purpose of this thesis was to determine the feasibility of employing SCRAMJET technology for an intermediate propulsive stage of an expendable launch vehicle. This was motivated by the fact that SCRAMJETS offer a very high propulsive efficiency when compared to conventional chemical rockets. The incorporation of a SCRAMJET engine into the configuration stack' of an expendable launch vehicle, offers the promise of increased payload mass fraction or an increase in the number of attainable orbital profiles. Analytical tools were developed using open-source software to identify launch trajectories for the SCRAMJET-enabled rocket configurations, and to determine how these would differ from conventional launch profiles. The effects of incremental increases in configuration lift and drag coefficients due to the SCRAMJET stage was analyzed. It was determined that incorporation of SCRAMJET Technology into an expendable rocket configuration offered marked improvement in performance, reduction in total launch weight, and increase operational flexibility when compared to a similarly sized conventional chemical rocket.

Download or read book A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs written by National Research Council and published by National Academies Press. This book was released on 2007-01-14 with total page 288 pages. Available in PDF, EPUB and Kindle. Book excerpt: Rocket and air-breathing propulsion systems are the foundation on which planning for future aerospace systems rests. A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs assesses the existing technical base in these areas and examines the future Air Force capabilities the base will be expected to support. This report also defines gaps and recommends where future warfighter capabilities not yet fully defined could be met by current science and technology development plans.

Download or read book Two stage Reusable Launch System Utilizing a Winged Core Vehicle and Glideback Boosters written by and published by . This book was released on 1989 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Rocket based Combined Cycle Reusable Launch Vehicles written by Ronald S. Fry and published by . This book was released on 1995 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Modern Engineering for Design of Liquid Propellant Rocket Engines written by Dieter K. Huzel and published by AIAA. This book was released on 1992 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Systems Analysis of Future Space Launch Requirements and Capabilities written by Norman F. Thompson (CAPT, USAF., III) and published by . This book was released on 1985 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: