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Atlas Launch System Mission Planner's Guide, Atlas V Addendum
ATLAS Atlas Launch System Mission Planner’s Guide, Atlas V Addendum FOREWORD This Atlas V Addendum supplements the current version of the Atlas Launch System Mission Plan- ner’s Guide (AMPG) and presents the initial vehicle capabilities for the newly available Atlas V launch system. Atlas V’s multiple vehicle configurations and performance levels can provide the optimum match for a range of customer requirements at the lowest cost. The performance data are presented in sufficient detail for preliminary assessment of the Atlas V vehicle family for your missions. This guide, in combination with the AMPG, includes essential technical and programmatic data for preliminary mission planning and spacecraft design. Interface data are in sufficient detail to assess a first-order compatibility. This guide contains current information on Lockheed Martin’s plans for Atlas V launch services. It is subject to change as Atlas V development progresses, and will be revised peri- odically. Potential users of Atlas V launch service are encouraged to contact the offices listed below to obtain the latest technical and program status information for the Atlas V development. For technical and business development inquiries, contact: COMMERCIAL BUSINESS U.S. GOVERNMENT INQUIRIES BUSINESS INQUIRIES Telephone: (691) 645-6400 Telephone: (303) 977-5250 Fax: (619) 645-6500 Fax: (303) 971-2472 Postal Address: Postal Address: International Launch Services, Inc. Commercial Launch Services, Inc. P.O. Box 124670 P.O. Box 179 San Diego, CA 92112-4670 Denver, CO 80201 Street Address: Street Address: International Launch Services, Inc. Commercial Launch Services, Inc. 101 West Broadway P.O. Box 179 Suite 2000 MS DC1400 San Diego, CA 92101 12999 Deer Creek Canyon Road Littleton, CO 80127-5146 A current version of this document can be found, in electronic form, on the Internet at: http://www.ilslaunch.com ii ATLAS LAUNCH SYSTEM MISSION PLANNER’S GUIDE ATLAS V ADDENDUM (AVMPG) REVISIONS Revision Date Rev No. -
Launch Options for the Future: a Buyer's Guide (Part 7 Of
— Chapter 3 Enhanced Baseline CONTENTS , Page Improving the Shuttle . 27 Advanced Solid Rocket Motors (ASRMs) . 27 Liquid Rocket Boosters (LRBs) . 28 Lighter Tanks . 29 Improving Shuttle Ground Operations . 29 Improving Existing ELVs . 29 Delta . 30 Atlas-Centaur . ● ● . .* . 30 Titan . ● . ✎ ✎ . 30 Capability . ✎ . ✎ ✎ . ● ✎ ✎ . 30 Table 3-1. Theoretical Lift Capability of Enhanced U.S. Launch Systems. 31 Chapter 3 Enhanced Baseline The ENHANCED BASELINE option is the U.S. Government’s “Best Buy” if . it desires a space program with current or slightly greater levels of activity. By making in- cremental improvements to existing launch vehicles, production and launch facilities, the U.S. could increase its launch capacity to about 1.4 million pounds per year to LEO. The investment required would be low compared to building new vehicles; however, the ade- quacy of the resulting fleet resiliency and dependability is uncertain. This option would not provide the low launch costs (e.g. 10 percent of current costs) sought for SDI deploy- ment or an aggressive civilian space initiative, like a piloted mission to Mars, IMPROVING THE SHUTTLE The Shuttle, though a remarkable tech- . reducing the number of factory joints and nological achievement, never achieved its in- the number of parts, tended payload capacity and recent safety . designing the ASRMs so that the Space modifications have further degraded its per- Shuttle Main Engines no longer need to formance by approximately 4,800 pounds. be throttled during the region of maxi- Advanced Solid Rocket Motors (ASRMs) or mum dynamic pressure, Liquid Rocket Boosters (LRBs) have the potential to restore some of this perfor- ● replacing asbestos-bearing materials, mance; studies on both are underway. -
N AS a Facts
National Aeronautics and Space Administration NASA’s Launch Services Program he Launch Services Program (LSP) manufacturing, launch operations and rockets for launching Earth-orbit and Twas established at Kennedy Space countdown management, and providing interplanetary missions. Center for NASA’s acquisition and added quality and mission assurance in In September 2010, NASA’s Launch program management of expendable lieu of the requirement for the launch Services (NLS) contract was extended launch vehicle (ELV) missions. A skillful service provider to obtain a commercial by the agency for 10 years, through NASA/contractor team is in place to launch license. 2020, with the award of four indefinite meet the mission of the Launch Ser- Primary launch sites are Cape Canav- delivery/indefinite quantity contracts. The vices Program, which exists to provide eral Air Force Station (CCAFS) in Florida, expendable launch vehicles that NASA leadership, expertise and cost-effective and Vandenberg Air Force Base (VAFB) has available for its science, Earth-orbit services in the commercial arena to in California. and interplanetary missions are United satisfy agencywide space transporta- Other launch locations are NASA’s Launch Alliance’s (ULA) Atlas V and tion requirements and maximize the Wallops Flight Facility in Virginia, the Delta II, Space X’s Falcon 1 and 9, opportunity for mission success. Kwajalein Atoll in the South Pacific’s Orbital Sciences Corp.’s Pegasus and facts The principal objectives of the LSP Republic of the Marshall Islands, and Taurus XL, and Lockheed Martin Space are to provide safe, reliable, cost-effec- Kodiak Island in Alaska. Systems Co.’s Athena I and II. -
Launch Options for the Future: a Buyer's Guide
Launch Options for the Future: A Buyer's Guide July 1988 NTIS order #PB89-114268 Recommended Citation: U.S. Congress, Office of Technology Assessment, Launch Options for the Future: Buyer’s Guide, OTA-ISC-383 (Washington, DC: U.S. Government Printing Office, July 1988). Library of Congress Catalog Card Number 88-600540 For sale by the Superintendent of Documents U.S. Government Printing Office, Washington, DC 20402-9325 (order form can be found in the back of this report) Foreword Adequate, reliable space transportation is the key to this Nation’s future in space. Over the next several years, Congress must make critical decisions regarding the direction and funding of U.S. space transportation systems. These decisions include improving existing launch sys- tems, designing and procuring new launch systems, and developing advanced technologies. America’s constrained budgetary environment and the lack of a national consensus about the future of the U.S. space program make Congress’s role in this process more difficult and im- portant than ever. In order to decide which paths to take in space transportation, Congress must first decide what it wants to do in space and what it can afford. A space transportation system designed to meet current needs would be woefully inadequate to support a piloted mission to the planet Mars or to deploy ballistic missile defenses. Accordingly, this special report, which is part of a broader assessment of space transportation requested by the House Committee on Science, Space, and Technology, and the Senate Committee on Commerce, Science, and Transporta- tion, takes the form of a “buyer’s guide” to space transportation. -
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. -
The 6555Th Table of Contents
The 6555th Table of Contents The 6555th Missile and Space Launches Through 1970 by Mark C. Cleary 45th Space Wing History Office Table of Contents Preface Chapter I - Foundations of the 6555th: The Post War Legacy Section 1 - Post-War legacy Through 1949 Section 2 - Activities at Holloman, Eglin and Patrick AFB, 1950-1951 Chapter II - MATADOR and the Era of Winged Missiles Section 1 - MATADOR Operations Through 1954 Section 2 - MATADOR and MACE Operations 1955-1963 Section 3 - LARK, BOMARC and SNARK Operations Section 4 - The NAVAHO Program The 6555th Table of Contents Chapter III - The 6555th's Role in the Development of Ballistic Missiles Section 1 - Ballistic Missile Test Organizations and Commanders Section 2 - The Eastern Test Range in the 1950's Section 3 - Ballistic Missile Test Objectives Section 4 - The THOR Ballistic Missile Program Section 5 - The ATLAS Ballistic Missile Program Section 6 - The TITAN Ballistic Missile Program Section 7 - Organization, Resources and Activities in the 1960's Section 8 - The MINUTEMAN Ballistic Missile Development Program Chapter IV - Taking the High Ground: The 6555th's Role in Space Through 1970 Section 1 - U. S. Military Space Efforts Through 1960 Section 2 - ATLAS, THOR and BLUE SCOUT Space Operations Section 3 - The TITAN II/GEMINI Program Section 4 - The TITAN III Program Section 5 - Organizational Changes 1965-1970 Preface (1st Edition, November 1991) When I assumed the duties of Chief, ESMC History Office in January 1986, I was completely unaware of the 6555th's contributions to America's missile and space efforts in the 1950s and 1960s. Like most Americans -- indeed, like most people the world over -- I assumed that the National Aeronautics and Space Administration dominated most aspects of the United States space effort after 1958. -
Information Summary Assurance in Lieu of the Requirement for the Launch Service Provider Apollo Spacecraft to the Moon
National Aeronautics and Space Administration NASA’s Launch Services Program he Launch Services Program was established for mission success. at Kennedy Space Center for NASA’s acquisi- The principal objectives are to provide safe, reli- tion and program management of Expendable able, cost-effective and on-schedule processing, mission TLaunch Vehicle (ELV) missions. A skillful NASA/ analysis, and spacecraft integration and launch services contractor team is in place to meet the mission of the for NASA and NASA-sponsored payloads needing a Launch Services Program, which exists to provide mission on ELVs. leadership, expertise and cost-effective services in the The Launch Services Program is responsible for commercial arena to satisfy Agencywide space trans- NASA oversight of launch operations and countdown portation requirements and maximize the opportunity management, providing added quality and mission information summary assurance in lieu of the requirement for the launch service provider Apollo spacecraft to the Moon. to obtain a commercial launch license. The powerful Titan/Centaur combination carried large and Primary launch sites are Cape Canaveral Air Force Station complex robotic scientific explorers, such as the Vikings and Voyag- (CCAFS) in Florida, and Vandenberg Air Force Base (VAFB) in ers, to examine other planets in the 1970s. Among other missions, California. the Atlas/Agena vehicle sent several spacecraft to photograph and Other launch locations are NASA’s Wallops Island flight facil- then impact the Moon. Atlas/Centaur vehicles launched many of ity in Virginia, the North Pacific’s Kwajalein Atoll in the Republic of the larger spacecraft into Earth orbit and beyond. the Marshall Islands, and Kodiak Island in Alaska. -
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. -
Universal Small Payload Interface – an Assessment of US Piggyback Launch Capability
SSC00-XI-3 Universal Small Payload Interface – An Assessment of US Piggyback Launch Capability Shahed Aziz AeroAstro, Inc. 327 A Street, 5th Floor Boston, MA 02210 (617) 451-8630 [email protected] Paul Gloyer AeroAstro, Inc. Bldg 8201, Room 209 Stennis Space Center, MS 39529 (228) 688-2790 [email protected] Joel Pedlikin AeroAstro, Inc. 327 A Street, 5th Floor Boston, MA 02210 (617) 451-8630 [email protected] Kimberly Kohlhepp AeroAstro, Inc. 327 A Street, 5th Floor Boston, MA 02210 (617) 451-8630 [email protected] Abstract. Small satellites are becoming the solution of choice for planners trying to reduce space mission costs and shorten schedules. Secondary launches are a quick, frequent, low-cost, reliable solution for small satellites. Most international small spacecraft are launched as secondary piggyback payloads, aboard larger more efficient rockets. However, piggyback accommodations in the US are rare, done only on a case-by-case basis, and far from low cost. AeroAstro is presently developing the Universal Small Payload Interface (USPI), a standardized template for integrating and launching small spacecraft. It is designed so that mission developers can design to its requirements in order to be compatible on demand with a number of different secondary launch vehicle slots. The ‘Phase A’ USPI, based exclusively on existing secondary opportunities, will be complete by August 2000. Phases B and C, based on potential modifications of existing launch vehicles, will be complete by the end of the year. Missions will be quickly designed to a common interface standard, decreasing their dependence on a specific launch. When the spacecraft is ready, the next USPI launch available will be used, bringing ‘launch on-demand’ closer to reality. -
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.