LCD-79-112 Procurement of DSCS II Satellites F-17 and F-18
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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. -
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. -
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. -
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. -
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). -
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. -
Titan II Small Multisatellite Mission Approach
I I Titan II Small Multisatellite Mission Approach Aubrey J. Butts I David F. Giere Bruce M. French Martin Marietta Astronautics Group John J. Kusnierek I Space Systems Division, USAF At the present time, small satellite programs are faced with the dilemma that they are I sometimes so small that they cannot afford the expense of a dedicated Expendable Launch Vehicle (EL V) and. therefore, must attempt to find a way to get into orbit as a secondary payload. This paper discusses another alternative, the use of a Titan II as a dedicated launch vehicle for a group of small satellites. Launches could be scheduled on a periodic I basis as a function of predicted need. The Titan II has the capability of inserting total payload weight of 3,000 to 4,000 lbs. into high-inclination, low-earth orbits and smaller payloads to higher orbits. Orbit changes are possible depending on the altitudes and I payloads weights involved. Payload fairings are available for small and large payloads. Since the total payload could conceivably consist of satellites from several unrelated programs, some type of mission "broker" or central contracting agency would be needed to develop and implement a multisatellite mission. This paper offers an approach to I implementing a mission of this type that would allow small satellites to schedule a launch on the T -II multisatellite carrier at a predetermined launch date during each year. The costs would be shared between payloads on the basis of weight and volume. This gives those small satellite programs a launch option that would provide on-orbit operation at a I predetermined time. -
Up from Kitty Hawk Chronology
airforcemag.com Up From Kitty Hawk Chronology AIR FORCE Magazine's Aerospace Chronology Up From Kitty Hawk PART ONE PART TWO 1903-1979 1980-present 1 airforcemag.com Up From Kitty Hawk Chronology Up From Kitty Hawk 1980-1989 F-117 Nighthawk stealth fighters, first flight June 1981. Articles noted throughout the chronology are hyperlinked to the online archive for Air Force Magazine and the Daily Report. 1980 March 12-14, 1980. Two B-52 crews fly nonstop around the world in 43.5 hours, covering 21,256 statute miles, averaging 488 mph, and carrying out sea surveillance/reconnaissance missions. April 24, 1980. In the middle of an attempt to rescue US citizens held hostage in Iran, mechanical difficulties force several Navy RH-53 helicopter crews to turn back. Later, one of the RH-53s collides with an Air Force HC-130 in a sandstorm at the Desert One refueling site. Eight US servicemen are killed. Desert One May 18-June 5, 1980. Following the eruption of Mount Saint Helens in northwest Washington State, the Aerospace Rescue and Recovery Service, Military Airlift Command, and the 9th Strategic Reconnaissance Wing conduct humanitarian-relief efforts: Helicopter crews lift 61 people to safety, while SR–71 airplanes conduct aerial photographic reconnaissance. May 28, 1980. The Air Force Academy graduates its first female cadets. Ninety-seven women are commissioned as second lieutenants. Lt. Kathleen Conly graduates eighth in her class. Aug. 22, 1980. The Department of Defense reveals existence of stealth technology that “enables the United States to build manned and unmanned aircraft that cannot be successfully intercepted with existing air defense systems.” Sept. -
Draft Environmental Impact Statement for the Ulysses Mission (Tier 2)
NASA National Aeronautics and Space Administration February 1990 Draft Environmental Impact Statement for the Ulysses Mission (Tier 2) (_AgA-i'M-I02993) ORAF[ _-NVTRr_NM_TAL I-MPACT Nq0-]4777 STATEMEf'!T FDR THt ULYsSeS MTSSIqN (TIER 2) (NASA) 1_7 p C_EL. ]3? Draft Environmental Impact Statement for the Ulysses Mission (Tier 2) Office of Space Science and Applications Solar System Exploration Division Washington, DC 20546 February 1990 Copies of this document can be obtained from: NeUonel Technical Information Service (NTIS) 5285 Port Royal Road Springfield, VA 22161 Phone: (703) 487-4650 For Rush Orders: (703) 4874700 Request the document as: N90-14727 ABSTRACT LEAD AGENCY: National Aeronautics and Space Administration Washington, DC 20546 COOPERATING AGENCY: U.S. Department of Energy Washington, DC 20585 FOR INFORMATION CONTACT: Dr. Dudley G. McConnell NASA Headquarters Code EL Washington, DC 20546 (202) 453-1587 DATE: February 1990 This Draft Environmental Impact Statement (DEIS) addresses the environmental impacts which may be caused by the implementation of a space flight mission to observe the polar regions of the Sun. The proposed action is completing the preparation and operation of the Ulysses spacecraft, including its planned launch on the Space Transportation System (STS) Shuttle in October 1990 or in the backup opportunity in November 1991, and the alternative of canceling further work on the mission. The Tier I EIS (NASA 1988a) included a delay alternative which considered the Titan IV launch vehicle as an alternative booster stage for launch in 1991 or later. However, in November 1988, the U.S. Air Force, which procures the Titan IV, notified the National Aeronautics and Space Administration (NASA) that it could not provide a Titan IV vehicle for the 1991 launch opportunity because of high priority Department of Defense requirements. -
Table of Contents
THE CAPE Military Space Operations 1971-1992 by Mark C. Cleary 45th Space Wing History Office Table of Contents Preface Chapter I -USAF Space Organizations and Programs Table of Contents Section 1 - Air Force Systems Command and Subordinate Space Agencies at Cape Canaveral Section 2 - The Creation of Air Force Space Command and Transfer of Air Force Space Resources Section 3 - Defense Department Involvement in the Space Shuttle Section 4 - Air Force Space Launch Vehicles: SCOUT, THOR, ATLAS and TITAN Section 5 - Early Space Shuttle Flights Section 6 - Origins of the TITAN IV Program Section 7 - Development of the ATLAS II and DELTA II Launch Vehicles and the TITAN IV/CENTAUR Upper Stage Section 8 - Space Shuttle Support of Military Payloads Section 9 - U.S. and Soviet Military Space Competition in the 1970s and 1980s Chapter II - TITAN and Shuttle Military Space Operations Section 1 - 6555th Aerospace Test Group Responsibilities Section 2 - Launch Squadron Supervision of Military Space Operations in the 1990s Section 3 - TITAN IV Launch Contractors and Eastern Range Support Contractors Section 4 - Quality Assurance and Payload Processing Agencies Section 5 - TITAN IIIC Military Space Missions after 1970 Section 6 - TITAN 34D Military Space Operations and Facilities at the Cape Section 7 - TITAN IV Program Activation and Completion of the TITAN 34D Program Section 8 - TITAN IV Operations after First Launch Section 9 - Space Shuttle Military Missions Chapter III - Medium and Light Military Space Operations Section 1 - Medium Launch Vehicle and Payload Operations Section 2 - Evolution of the NAVSTAR Global Positioning System and Development of the DELTA II Section 3 - DELTA II Processing and Flight Features Section 4 - NAVSTAR II Global Positioning System Missions Section 5 - Strategic Defense Initiative Missions and the NATO IVA Mission Section 6 - ATLAS/CENTAUR Missions at the Cape Section 7 - Modification of Cape Facilities for ATLAS II/CENTAUR Operations Section 8 - ATLAS II/CENTAUR Missions Section 9 - STARBIRD and RED TIGRESS Operations Section 10 - U.S. -
In Better Times, Martin Marietta Titan 340 Ex- Pendable Launch Vehi- Cle (ELV) Lifts Off with Spacebound Military Payload
In better times, Martin Marietta Titan 340 Ex- pendable Launch Vehi- cle (ELV) lifts off with spacebound military payload. Successive Titan 340 failures bracketed the destruc- tion of Space Shuttle Challenger. putting USAF's space-launch program on hold last year. Things are looking up, now that Air Force Systems Command's Space Division has con- ducted its Titan 340 in- spection and recovery program and has put into effect its compre- hensive space-launch recovery plan. leading to a better mix of booster rockets to augment the Shuttles in assuring fu- ture US access to space. Mr HE US space program is begin- Vital military pay- ning to lose the snakebitten look loads are still on the it took on last year amid a shocking succession of accidents befalling ground, but USAF is Space Shuttle Challenger and three unmanned launch vehicles. rebuilding its launch The program still has a long, long capability to be way to go in fully recovering from the impact of those accidents. They stronger and more left the Air Force incapable of versatile than that of launching growing numbers of satel- lites vital to national security. the pre-Challenger This sobering—even scary— state of affairs will persist into next era. year and will not be much alleviated for another year or so after that. Shuttle Orbiters will not fly again until February 1988, at the earliest. The first of the big Titan IV Comple- mentary Expendable Launch Vehi- cles (CELVs) now being developed to carry outsized payloads high into Coming space will not be ready for launch until early 1989. -
Read the Spaceport News Print Edition (PDF)
Oct. 1, 2008 Vol. 48, No. 20 NASA celebrates 50th Anniversary ct. 1 marks the 50th the STS-125 Hubble Space Anniversary of Director’s Note Telescope servicing mission. NASA as it was on Over Hubble’s 18 year O By Bill history, many extraordinary this date in 1958 that the Na- Parsons tional Aeronautics and Space discoveries have been Director, made by what this amazing Administration began opera- Kennedy tions. Over the past 50 years, Space instrument has captured. We the employees of America’s Center also are preparing for the space program have been at upcoming missions to the the forefront of many incred- I mention this historic date International Space Station ible accomplishments. because once again we are and preparing for launches Kennedy Space Center preparing to go back to the through the Launch Services has a rich history in the space moon. This time, we are Program. Our Constellation program having been named going to stay. We will have Program work is moving ahead, and we are preparing an independent NASA a sustained human presence. for the Ares I-X test fl ight installation in 1962. NASA is a forward-looking next year. From the historic launch agency, and this is our future. In the short history of pads here in Florida, we NASA’s 50th NASA, numerous benefi ts to have launched missions Anniversary is a historic society have come through of discovery. Next year, milestone that gives us an the work of America’s we will celebrate the 40th opportunity to refl ect on past space program.