Characterizing GEO Titan IIIC Transtage Fragmentations Using
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L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
Paper Session I-C - Delta II Development and Flight Results
1991 (28th) Space Achievement: A Global The Space Congress® Proceedings Destiny Apr 23rd, 2:00 PM - 5:00 PM Paper Session I-C - Delta II Development and Flight Results Sam K. Mihara McDonnell Douglas Space Systems Company, Huntington Beach, CA Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Mihara, Sam K., "Paper Session I-C - Delta II Development and Flight Results" (1991). The Space Congress® Proceedings. 7. https://commons.erau.edu/space-congress-proceedings/proceedings-1991-28th/april-23-1991/7 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. MDC91H1017 APRIL 1991 DELTA II (MODEL 7925) DEVELOPMENT AND FLIGHT RESULTS S.K. MIHARA Presented to Twenty-Eighth Space Congress Cocoa Beach, Florida April 1991 McDonnell Douglas Space Systems Company /tfCDO/V/V^f.1. DOUGLAS a-to DELTA II (MODEL 7925) DEVELOPMENT AND FLIGHT RESULTS S.K. MIHARA* ABSTRACT This paper describes the design changes to the latest Delta Launch vehicle. Delta II Model 7925, The results of developments on five main subsystems are described. The paper includes the flight results of Delta II launches to date. DELTA HISTORY The McDonnell Douglas Space Systems Company (MDSSC) Delta launch vehicle has been a NASA space "workhorse" for 31 years. It had its beginnings in the mid-1950s with the Thor vehicle. Subsequently, the NASA Goddard Space Flight Center contracted for the development of an interim space launch vehicle using a modified Thor first stage with Vanguard missile components for the second and third stages. -
10/2/95 Rev EXECUTIVE SUMMARY This Report, Entitled "Hazard
10/2/95 rev EXECUTIVE SUMMARY This report, entitled "Hazard Analysis of Commercial Space Transportation," is devoted to the review and discussion of generic hazards associated with the ground, launch, orbital and re-entry phases of space operations. Since the DOT Office of Commercial Space Transportation (OCST) has been charged with protecting the public health and safety by the Commercial Space Act of 1984 (P.L. 98-575), it must promulgate and enforce appropriate safety criteria and regulatory requirements for licensing the emerging commercial space launch industry. This report was sponsored by OCST to identify and assess prospective safety hazards associated with commercial launch activities, the involved equipment, facilities, personnel, public property, people and environment. The report presents, organizes and evaluates the technical information available in the public domain, pertaining to the nature, severity and control of prospective hazards and public risk exposure levels arising from commercial space launch activities. The US Government space- operational experience and risk control practices established at its National Ranges serve as the basis for this review and analysis. The report consists of three self-contained, but complementary, volumes focusing on Space Transportation: I. Operations; II. Hazards; and III. Risk Analysis. This Executive Summary is attached to all 3 volumes, with the text describing that volume highlighted. Volume I: Space Transportation Operations provides the technical background and terminology, as well as the issues and regulatory context, for understanding commercial space launch activities and the associated hazards. Chapter 1, The Context for a Hazard Analysis of Commercial Space Activities, discusses the purpose, scope and organization of the report in light of current national space policy and the DOT/OCST regulatory mission. -
A Breath of Fresh Air: Air-Scooping Electric Propulsion in Very Low Earth Orbit
A BREATH OF FRESH AIR: AIR-SCOOPING ELECTRIC PROPULSION IN VERY LOW EARTH ORBIT Rostislav Spektor and Karen L. Jones Air-scooping electric propulsion (ASEP) is a game-changing concept that extends the lifetime of very low Earth orbit (VLEO) satellites by providing periodic reboosting to maintain orbital altitudes. The ASEP concept consists of a solar array-powered space vehicle augmented with electric propulsion (EP) while utilizing ambient air as a propellant. First proposed in the 1960s, ASEP has attracted increased interest and research funding during the past decade. ASEP technology is designed to maintain lower orbital altitudes, which could reduce latency for a communication satellite or increase resolution for a remote sensing satellite. Furthermore, an ASEP space vehicle that stores excess gas in its fuel tank can serve as a reusable space tug, reducing the need for high-power chemical boosters that directly insert satellites into their final orbit. Air-breathing propulsion can only work within a narrow range of operational altitudes, where air molecules exist in sufficient abundance to provide propellant for the thruster but where the density of these molecules does not cause excessive drag on the vehicle. Technical hurdles remain, such as how to optimize the air-scoop design and electric propulsion system. Also, the corrosive VLEO atmosphere poses unique challenges for material durability. Despite these difficulties, both commercial and government researchers are making progress. Although ASEP technology is still immature, it is on the cusp of transitioning between research and development and demonstration phases. This paper describes the technical challenges, innovation leaders, and potential market evolution as satellite operators seek ways to improve performance and endurance. -
The Delta Launch Vehicle- Past, Present, and Future
The Space Congress® Proceedings 1981 (18th) The Year of the Shuttle Apr 1st, 8:00 AM The Delta Launch Vehicle- Past, Present, and Future J. K. Ganoung Manager Spacecraft Integration, McDonnell Douglas Astronautics Co. H. Eaton Delta Launch Program, McDonnell Douglas Astronautics Co. Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Ganoung, J. K. and Eaton, H., "The Delta Launch Vehicle- Past, Present, and Future" (1981). The Space Congress® Proceedings. 7. https://commons.erau.edu/space-congress-proceedings/proceedings-1981-18th/session-6/7 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. THE DELTA LAUNCH VEHICLE - PAST, PRESENT AND FUTURE J. K. Ganoung, Manager H. Eaton, Jr., Director Spacecraft Integration Delta Launch Program McDonnell Douglas Astronautics Co. McDonnell Douglas Astronautics Co. INTRODUCTION an "interim space launch vehicle." The THOR was to be modified for use as the first stage, the The Delta launch vehicle is a medium class Vanguard second stage propulsion system, was used expendable booster managed by the NASA Goddard as the Delta second stage and the Vanguard solid Space Flight Center and used by the U.S. rocket motor became Delta's third stage. Government, private industry and foreign coun Following the eighteen month development program tries to launch scientific, meteorological, and failure to launch its first payload into or applications and communications satellites. -
IUS/TUG ORBITAL OPERATIONS and MISSION SUPPORT STUDY FINAL REPORT
https://ntrs.nasa.gov/search.jsp?R=19750016720 2020-03-22T21:57:01+00:00Z Prepared for the MAY, 1975 GEORGE C MARSHALL SPACE FLIGHT CENTER Contract No NAS8-31009 Huntsville, Alabama IBM No 75W-00072 IUS/TUG ORBITAL OPERATIONS and MISSION SUPPORT STUDY FINAL REPORT Vol V of V - Cost Estimates (NASA-CR-143857) TUS/TUG ORBITAL OPEFATIONS N75-24792 AND M-ISSION SUPPORT STUDY. VOLUME 5: COST ESTI ATES Final Report (Internattonal Business Machines Corp.) 184 p HC $7.00 Unclas CSCL 22A G3/13 26227 Prepared for the MAY, 1975 GEORGE C MARSHALL SPACE FLIGHT CENTER Contract No NAS8-31009 Huntsville, Alabama IBM No 75W-00072 IUS/TUG ORBITAL OPERATIONS and MISSION SUPPORT STUDY FINAL REPORT Vol V of V - Cost Estimates Classification and Content Approval - '- Data Manager Approval Z2 Program Office Approval zC7 !4 PHILCO 490 Phico Fcrd Corporation Federal Systems Division, Space Systems/Huntsville, AlabmaWestr eopme Laorories son FOREWORD This final report of the IUS/Tug Orbital Operations and Mission Study was prepared for the National Aeronautics and Space Administration, George C Marshall Space Flight Center by the IBM Corporation in accordance with Contract NAS8-31009 The study effort described herein was conducted under the direction of NASA Contract Officer's Representative (COR), Mr. Sidney P Saucier This report was prepared by the IBM Corporation, Federal Systems Division, Huntsville, Alabama, under the direction of Mr Roy E Day, IBM Study Manager Technical support was provided to IBM by the Philco-Ford Corporation, Western Development Laboratories Division, Palo Alto, California, under the direction of Dr W E Waters, Philco-Ford Study Manager The study results were developed during the period from dune, 1974, through February, 1975, with the final report being distributed in May, 1975. -
George C. Marshall Space Flight Center Malshall Space Flight Center, Alabama
NASA TECHNICAL MEMORANDUM NASA TM X-53973 SPACE FLIGHT EVOLUTION By Georg von Tiesenhausen and Terry H. Sharpe Advanced Systems Analysis Office June 30,1970 NASA George C. Marshall Space Flight Center Malshall Space Flight Center, Alabama MSFC - Form 3190 (September 1968) j NASA TM X-53973 I [. TITLE AND SUBTITLE 5. REPORT DATE June 30,1970 Space Flight Evolution 6. PERFORMlNG ORGANIZATION CODE PD-SA 7. AUTHOR(S) 8. PERFORMING ORGANIZATION REPORT # Georg von Tiesenhausen and Terry H. Sharpe I 3. PERFORMlNG ORGANIZATION NAME AND ADDRESS lo. WORK UNIT, NO. Advanced Systems Analysis Office Program Development 1 1. CONTRACT OR GRANT NO. Marshall Space Flight Center, Alabama 35812 13. TYPE OF REPORT & PERIOD COVEREC 2. SPONSORING AGENCY NAME AND ADDRESS Technical Memorandum 14. SPONSORING AGENCY CODE I 15. SUPPLEMENTARY NOTES 16. ABSTRACT This report describes a possible comprehensive path of future, space flight evolution. The material in part originated from earlier NASA efforts to defme a space program in which earth orbital, lunar, and planetary programs are integrated. The material presented is not related to specific time schedules but provides an evolutionary sequence. The concepts of commonality of hardware and reusability of systems are introduced as keys to a low cost approach to space flight. The verbal descriptions are complemented by graphic interpretations in order to convey a more vivid impression of the concepts and ideas which make upthis program. 17. KEY WORDS 18. DISTRIBUTION STATEMENT STAR Announcement Advanced Systems Analysis Office 19. SECURITY CLASSIF. (of this rePmt> (20. SECURITY CLA ;IF. (of this page) 121. NO. OF PAGES 122. -
Characterization of Spacecraft Materials Using Reflectance Spectroscopy
Characterization of spacecraft materials using reflectance spectroscopy Jacqueline A. Reyes University of Texas at El Paso-Jacobs JETS Contract, El Paso, TX 79968 Darren Cone University of Texas at El Paso, El Paso, TX 79968 ABSTRACT Materials interact with light in a unique manner due to their individual elemental composition. Elements emit different light energies that fall within the electromagnetic spectrum, therefore corresponding to a specified wavelength per element. The reflectance spectrum produced from common spacecraft materials can be used to assist with remote orbital debris material identification techniques and can be further related to debris albedo and size. Materials used in aerospace design, such as aluminum alloys, stainless steels, ceramics, silicone paints, and solar cells, have been substantially characterized using reflectance spectroscopic techniques. An Analytical Spectral Device (ASD) was utilized to perform characterization on various spacecraft and rocket body structures by producing a spectrum relatively unique to a material from its properties in response to light. The materials used as specimen for this investigation specifically belong to a Titan IIIC Transtage test article rocket body, stainless steel radar calibration spheres, and solar cells used to construct a Hughes/Boeing HS-376 spacecraft. The spectrum results of said materials are presented in the subsequent work to enhance current spectroscopic data of interest within aerospace and orbital debris communities. 1. INTRODUCTION The space industry has succeeded in launching various spacecraft into Earth orbit to explore the nature of our space environment. This originated with the launch of the first satellite, Sputnik, on October 4, 1957 [1]. Since then, multiple space missions have been executed, leaving our near-Earth space environment populated with spacecraft. -
Date. Projeed Future NASA Programs Planned for the 1970'S Are Discussed Under the Headings Skylab, Space Shuttle, and Space Station
DOCURENT RESUME ED 050 993 SE 011 364 AUTHOR Froehlich, Walter TITLE Man in Space, Space in the Seventies. 7MSTITUTION National Aeronautics and Space Administration, Washington, D.C. REPORT NO EP-B1 PUB DATE Jan 71 NOTE 31p. AVAILABLE FROM Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 ($1.00) . EDRS PRICE EDRS Price MF-$0.35 HC riot Available from EDRS. DESCRIPTORS Aerospace Technology, *Program rescriptions, *Resource Materials, *Space, *State Agencies IDENTIFIERS National Aeronautics and Space Administration ABSTRACT Included is a summary of the Apollo lunar program to date. Projeed future NASA programs planned for the 1970's are discussed under the headings Skylab, Space Shuttle, and Space Station. Possibilities for the 1980's are outlined in the final section. (Author/AL) JUN 2 1 U.S. DEPARTMENT OF HEALTH, EDUCATION . " & WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS SEEN REPRODUCED EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIGINATING IT. POINTS OF VIEW OR OPINIONS STATED DO NOT NECES SARILY REPRESENT OFFICIAL OFFICE OF EOU MAN IN SPACE CATION POSITION OR POLICY Space In The Seventies Ilk National Aeronautics and Space Administration SPACE IN THE SEVENTIES Man has walked on the Moon, made scientific observations there, and brought back to Earth samples of the lunar surface. Unmanned scientific spacecraft have probed for facts about matter, radiation and magnetism in space, and have collected data relating to the Moon, Venus, Mars, the Sun and some of the stars, and reported their findings to ground stations on Earth. Spacecraft have been put into orbit around the Earth as weather observation stations, as communications relay stations for a world-wide telephone and television network, and as aids to navigation, In addition, the space program has accelerated the advance of technology for science and industry, contributing many new ideas, processes and materials. -
BELLCOMM, INC. Case 720 23 P Unclas
3 e--* I ', - -,p. .. - BELLCOMM, INC. 1100 Seventeenth Street, N.W. WkhingtoL D. C. 20036 SUBJECT: Selected Comments on Agena and DATE: March 26, 1968 Titan I11 Family Stages Case 720 FROM: C. Bendersky ABSTRACT This memo presents (unclassified) comments on the status of Lockheed Agena and Titan I11 family propulsion stages gathered to support current NASA Orbital Workshop Studies. (VASA-CR-955 11) SELECTED COMMENTS ON AGENA N79-72086 AND TITAN 3 FAHILY STAGES (Eellcomrn, Inc-) 23 P Unclas 00/75 11184 BELLCOMM,INC. 1100 Seventeenth Street, N.W. Washington, D. C. 20036 SUBJECT: Selected Comments on Agena and DATE: March 26, 1968 Titan I11 Family Stages Case 720 FROM: C. Bendersky MEMORANDUM FOR FILE This memo presents (unclassified) comments on the status of both the Lockheed Agena Space Propulsion Systems and the Martin Titan I11 booster family. The data presented were primarily obtained during a visit to Lockheed, Sunnyvale, Cali- fornia, January 23 and Martin, Denver, Colorado, January 24-25, 1968l. H. S. London was present 3t Martin. This memo will dis- cuss specific operational features of the subject stages of cur- rent interest to the hlorkshop B & C study. The detailed charac- teristics of the stases and flight performance data are available upon request from this writer. This memo reports information available as of February 1, 1968 and will be updated as warranted. 1.0 AGENA STAGES It must be emphasized that the available Aaena has achieved a high degree of reliability through flights on Thor, Atlas and Titan boosters. For example, more than 10 Titan IIIB/ Agenas have been successfully flown from the Western Test Range (NTR). -
IAA Situation Report on Space Debris - 2016
IAA Situation Report on Space Debris - 2016 Editors: Christophe Bonnal Darren S. McKnight International A cadem y of A stronautics Notice: The cosmic study or position paper that is the subject of this report was approved by the Board of Trustees of the International Academy of Astronautics (IAA). Any opinions, findings, conclusions, or recommendations expressed in this report are those of the authors and do not necessarily reflect the views of the sponsoring or funding organizations. For more information about the International Academy of Astronautics, visit the IAA home page at www.iaaweb.org. Copyright 2017 by the International Academy of Astronautics. All rights reserved. The International Academy of Astronautics (IAA), an independent nongovernmental organization recognized by the United Nations, was founded in 1960. The purposes of the IAA are to foster the development of astronautics for peaceful purposes, to recognize individuals who have distinguished themselves in areas related to astronautics, and to provide a program through which the membership can contribute to international endeavours and cooperation in the advancement of aerospace activities. © International Academy of Astronautics (IAA) May 2017. This publication is protected by copyright. The information it contains cannot be reproduced without written authorization. Title: IAA Situation Report on Space Debris - 2016 Editors: Christophe Bonnal, Darren S. McKnight Printing of this Study was sponsored by CNES International Academy of Astronautics 6 rue Galilée, Po Box 1268-16, 75766 Paris Cedex 16, France www.iaaweb.org ISBN/EAN IAA : 978-2-917761-56-4 Cover Illustration: NASA IAA Situation Report on Space Debris - 2016 Editors Christophe Bonnal Darren S. -
Titan Iv Requirements
OFFICE OF THE INSPECTOR GENERAL TITAN IV REQUIREMENTS Report No. 94-089 April 21, 1994 Department of Defense Additional Copies To obtain additional copies of this report, contact the Secondary Reports Distribution Unit, Audit Planning and Technical Support Directorate, at (703) 614-6303 (DSN 224-6303) or FAX (703) 614-8542. Suggestions for Future Audits To suggest ideas for or to request future audits, contact the Planning and Coordination Branch, Audit Planning and Technical Support Directorate, at (703) 614-1868 (DSN 224-1868) or FAX (703) 614-8542. Ideas and requests can also be mailed to: Inspector General, Department of Defense OAIG-AUD (ATTN: APTS Audit Suggestions) 400 Army Navy Drive (Room 801) Arlington, Virginia 22202-2884 DoD Hotline To report fraud, waste, or abuse, call the DoD Hotline at (800) 424-9098 (DSN 223-5080) or write to the DoD Hotline, The Pentagon, Washington, D.C. 20301-1900. The identity of writers and callers is fully protected. Acronyms FYDP Future Years Defense Program IV&V Independent Verification and Validation OSD Office of the Secretary of Defense RFP Request for Proposal SLAG Space Launch Advisory Group SPO System Program Office SRM Solid Rocket Motor SRMU Solid Rocket Motor Upgrade INSPECTOR GENERAL DEPARTMENT OF DEFENSE 400 ARMY NAVY DRIVE ARLINGTON, VIRGINIA 22202-2884 April 21, 1994 MEMORANDUM FOR ASSISTANT SECRETARY OF THE AIR FORCE (FINANCIAL MANAGEMENT AND COMPTROLLER) SUBJECT: Audit Report on Titan IV Requirements (Report No. 94-089) We are providing this audit report for your review and comments. It discusses requirements for the Titan IV expendable launch vehicle and for independent validation and verification of critical computer resources.