DOCSLIB.ORG

Athena Ic and Iic Space Launch Vehicles

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Athena Ic and Iic Space Launch Vehicles Athena Ic and IIc Space Launch Vehicles Lockheed Martin Alliant Techsystems (ATK) Gregory Kehrl Matt Steele 303-514-9548 801-251-3540 [email protected] [email protected] ©2010 Lockheed Martin Corporation/Alliant Techsystems (ATK) 04/10 Athena Ic and IIc Are Uniquely Suited for DoD and Civil Missions 92-in. Payload The two-stage Athena Ic and Fairing three-stage Athena IIc launch Payload vehicles incorporate the flight- Adapter proven CASTOR 120® first Orbit Adjust and second stages with the new Module CASTOR 30® upper stage and CASTOR 30® upgrades to electronic systems. Upper The Lockheed Martin/ATK team bring their unmatched depth and experience to this new partnership. Drawing on over Interstage 40 years of experience with expendable launch vehicle systems, the Athena team provides a reliable and cost-effective means Lunar- and multi-satellite capability to precisely deliver small payloads to Earth orbit. Both Athena Ic Modernized CASTOR 120® Second Stage and IIc provide a 92-in. payload Athena Ic and IIc Space Launch Vehicles fairing that accommodates a wide range Lockheed Martin Corporation and O 1,016 (40) of spacecraft: Alliant Techsystems (ATK) have teamed to Athena Provides Lower 2,029 2,017 NASA’s Lunar offer launch services utilizing upgraded and Interstage (79.9) O 1,026 (79.4) Unique Customer Benefits (40.4) Prospector modernized Athena rockets. • 100% domestic content improves sustained availability with TLI stage • Inherent simplicity increases reliability and NASA’s Based on the flight-proven Athena Ic O 2,103 • Responsiveness: (82.8) Kodiak Star, a and Athena IIc, these vehicles are designed to O 2,108 – 99% probability of favorable winds aloft at launch vs 25% (83.0) multiple payload provide reliable access to space for small CASTOR 120® 2,276 2,263 mission, shown for liquid propulsion systems (89.6) (89.1) payloads to a wide range of orbits. First Stage above. Flight – Faster launch recycle time than liquid propulsion proven payload The Athena launch vehicle family • Lowest Life Cycle Cost of all propulsion options adapters include – Long-term storage with minimal maintenance combines both companies’ heritage and CASTOR 30® static fire success M66 PLA 38-in., 47-in., – Low ground support and equipment infrastructure 66-in. and expertise to provide reliable launch services Dynamic Static requirements for maintenance and launch Envelope, Envelope, multi-satellite at an affordable price. mm (in.) mm (in.) dispensers. • Operational deployment demands Athena IIc Athena is available for launches – Easily maintained in a high state of readiness beginning in 2012, with a payload lift capability – Solid propulsion has decades of demonstrated 24/7 alert that supports NASA, the Department of Defense status capability (DoD) and commercial mission requirements. First-generation Athena I and II rockets became operational in 1995 and have flown seven times. Athena II launched the Lunar Prospector to the moon in 1998 and remains the only commercially developed launch vehicle to fly a lunar mission. Athena Ic and IIc Launch Vehicles Provide Assured Performance Athena Ic and IIc can be launched from multiple locations • Suborbital and ballistic lift capability available for special including Cape Canaveral Air Force Station, Kodiak customer needs such as test demonstrations. Launch Complex, Vandenberg Air Force Base, and NASA Wallops Mid-Atlantic Regional Spaceport. .
Load more

Recommended publications
  • Launch and Deployment Analysis for a Small, MEO, Technology Demonstration Satellite
    46th AIAA Aerospace Sciences Meeting and Exhibit AIAA 2008-1131 7 – 10 January 20006, Reno, Nevada Launch and Deployment Analysis for a Small, MEO, Technology Demonstration Satellite Stephen A. Whitmore* and Tyson K. Smith† Utah State University, Logan, UT, 84322-4130 A trade study investigating the economics, mass budget, and concept of operations for delivery of a small technology-demonstration satellite to a medium-altitude earth orbit is presented. The mission requires payload deployment at a 19,000 km orbit altitude and an inclination of 55o. Because the payload is a technology demonstrator and not part of an operational mission, launch and deployment costs are a paramount consideration. The payload includes classified technologies; consequently a USA licensed launch system is mandated. A preliminary trade analysis is performed where all available options for FAA-licensed US launch systems are considered. The preliminary trade study selects the Orbital Sciences Minotaur V launch vehicle, derived from the decommissioned Peacekeeper missile system, as the most favorable option for payload delivery. To meet mission objectives the Minotaur V configuration is modified, replacing the baseline 5th stage ATK-37FM motor with the significantly smaller ATK Star 27. The proposed design change enables payload delivery to the required orbit without using a 6th stage kick motor. End-to-end mass budgets are calculated, and a concept of operations is presented. Monte-Carlo simulations are used to characterize the expected accuracy of the final orbit.
    [Show full text]
  • 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.
    [Show full text]
  • Learning from Other People's Mistakes
    Learning from Other People’s Mistakes Most satellite mishaps stem from engineering mistakes. To prevent the same errors from being repeated, Aerospace has compiled lessons that the space community should heed. Paul Cheng and Patrick Smith he computer onboard the Clementine spacecraft froze immediately after a thruster was commanded to fire. A “watchdog” algorithm designed to stop “It’s always the simple stuff the thrusters from excessive firing could not execute, and CTlementine’s fuel ran out. !e mission was lost. Based on that kills you…. With all the this incident, engineers working on the Near Earth Asteroid Rendezvous (NEAR) program learned a key lesson: the testing systems, everything watchdog function should be hard-wired in case of a com- puter shutdown. As it happened, NEAR suffered a similar computer crash during which its thrusters fired thousands looked good.” of times, but each firing was instantly cut off by the still- —James Cantrell, main engineer operative watchdog timer. NEAR survived. As this example illustrates, insights from past anoma- for the joint U.S.-Russian Skipper lies are of considerable value to design engineers and other mission, which failed because program stakeholders. Information from failures (and near its solar panels were connected failures) can influence important design decisions and pre- vent the same mistakes from being made over and over. backward (Associated Press, 1996) Contrary to popular belief, satellites seldom fail because of poor workmanship or defective parts. Instead, most failures are caused by simple engineering errors, such as an over- looked requirement, a unit mix-up, or even a typo in a docu- ment.
    [Show full text]
  • Space Almanac 2007
    2007 Space Almanac The US military space operation in facts and figures. Compiled by Tamar A. Mehuron, Associate Editor, and the staff of Air Force Magazine 74 AIR FORCE Magazine / August 2007 Space 0.05g 60,000 miles Geosynchronous Earth Orbit 22,300 miles Hard vacuum 1,000 miles Medium Earth Orbit begins 300 miles 0.95g 100 miles Low Earth Orbit begins 60 miles Astronaut wings awarded 50 miles Limit for ramjet engines 28 miles Limit for turbojet engines 20 miles Stratosphere begins 10 miles Illustration not to scale Artist’s conception by Erik Simonsen AIR FORCE Magazine / August 2007 75 US Military Missions in Space Space Support Space Force Enhancement Space Control Space Force Application Launch of satellites and other Provide satellite communica- Ensure freedom of action in space Provide capabilities for the ap- high-value payloads into space tions, navigation, weather infor- for the US and its allies and, plication of combat operations and operation of those satellites mation, missile warning, com- when directed, deny an adversary in, through, and from space to through a worldwide network of mand and control, and intel- freedom of action in space. influence the course and outcome ground stations. ligence to the warfighter. of conflict. US Space Funding Millions of constant Fiscal 2007 dollars 60,000 50,000 40,000 30,000 20,000 10,000 0 Fiscal Year 59 62 65 68 71 74 77 80 83 86 89 92 95 98 01 04 Fiscal Year NASA DOD Other Total Fiscal Year NASA DOD Other Total 1959 1,841 3,457 240 5,538 1983 13,051 18,601 675 32,327 1960 3,205 3,892
    [Show full text]
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • NASA Launch Services Manifest
    Launch Options - Future Options • Constellation Architecture • Commercial Alternatives – SpaceX – Orbital Sciences • EELV Options • DIRECT • Side-Mount Shuttle Derived • Space (or “Senate”) Launch System • Recent Developments © 2012 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu U N I V E R S I T Y O F U.S. Future Launch Options MARYLAND 1 ENAE 791 - Launch and Entry Vehicle Design Attribution • Slides shown are from the public record of the deliberations of the Augustine Commission (2009) • Full presentation packages available at http:// www.nasa.gov/ofces/hsf/meetings/index.html U N I V E R S I T Y O F U.S. Future Launch Options MARYLAND 2 ENAE 791 - Launch and Entry Vehicle Design Review of Human Spaceflight Plans Constellation Overview June 17, 2009 Doug Cooke www.nasa.gov Jeff Hanley Constellation Architecture Earth Departure Stage Altair Lunar Lander Orion Ares I Crew Exploration Crew Launch Vehicle Vehicle Ares V Cargo Launch Vehicle Constellation is an Integrated Architecture National Aeronautics and Space Administration 2 Key Exploration Objectives 1. Replace Space Shuttle capability, with Shuttle retirement in 2010 2. To ensure sustainability, development and operations costs must be minimized 3. Develop systems to serve as building blocks for human exploration of the solar system using the Moon as a test bed 4. Design future human spaceflight systems to be significantly safer than heritage systems 5. Provide crew transport to ISS by 2015, to the lunar surface for extended durations by 2020, and to Mars by TBD 6. Separate crew from cargo delivery to orbit 7. Maintain and grow existing national aerospace supplier base 8.
    [Show full text]
  • By Matt Thompson and Theodore Reis
    MY BIG FAT GREEK DIVORCE TEN-MINUTE PLAY By Matt Thompson and Theodore Reis Copyright © MMVIII by Matt Thompson and Theodore Reis All Rights Reserved Heuer Publishing LLC, Cedar Rapids, Iowa The writing of plays is a means of livelihood. Unlawful use of a playwright’s work deprives the creator of his or her rightful income. The playwright is compensated on the full purchase price and the right of performance can only be secured through purchase of at least seven (7) copies of this work. PERFORMANCES ARE LIMITED TO ONE VENUE FOR ONE YEAR FROM DATE OF PURCHASE. The possession of this script without direct purchase from the publisher confers no right or license to produce this work publicly or in private, for gain or charity. On all programs and advertising this notice must appear: "Produced by special arrangement with Heuer Publishing LLC of Cedar Rapids, Iowa." This dramatic work is fully protected by copyright. No part of this work may be reproduced, stored in a retrieval system, or transmitted in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, without permission of the publisher. Copying (by any means) or performing a copyrighted work without permission constitutes an infringement of copyright. The right of performance is not transferable and is strictly forbidden in cases where scripts are borrowed or purchased second hand from a third party. All rights including, but not limited to the professional, motion picture, radio, television, videotape, broadcast, recitation, lecturing, tabloid, publication, and reading are reserved. COPYING OR REPRODUCING ALL OR ANY PART OF THIS BOOK IN ANY MANNER IS STRICTLY FORBIDDEN BY LAW.
    [Show full text]
  • Athena Mission Planner’S Guide (MPG)
    Athena Mission Planner’s Guide (MPG) Release Date Date – –2326 January August 2012 2011 Published by: Athena Mission Planner’s Guide FOREWORD January 2012 This Athena Mission Planner’s Guide presents information regarding the Athena Launch Vehicle and related launch services. A range of vehicle configurations and performance capabilities are offered to allow optimum match to customer requirements at low cost. Information is presented in sufficient detail for preliminary assessment of the Athena family for your missions. This guide includes essential technical and programmatic information for preliminary mission planning and preliminary spacecraft design. Athena performance capability, environments and interfaces are described in sufficient detail to assess a first-order compatibility. A description of the spacecraft processing and launch facilities at our launch sites is also included. This guide also describes the operations and hardware flow for the spacecraft and launch vehicle leading to encapsulation, spacecraft mating and launch. This guide is subject to change and will be revised periodically. For inquiries, contact: Gregory J. Kehrl Athena Mission Manager Telephone: (303) 977-0310 Fax: (303) 971-3748 E-mail: [email protected] Postal Address: Lockheed Martin Space Systems Company P.O. Box 179 Denver, CO 80201-0179 MS H3005 Street Address: Lockheed Martin Space Systems Company 12257 S. Wadsworth Blvd. Littleton, CO 80125 MS H3005 i Athena Mission Planner’s Guide TABLE OF CONTENTS 1.0 INTRODUCTION ..............................................................................................................
    [Show full text]
  • Access to Space
    databk7_collected.book Page 989 Monday, September 14, 2009 2:53 PM INDEX A (Office of Space Science), 585 Advanced Transportation Technology, 101 Academic programs, 10, 14 Advanced X-ray Astronomical Facility (AXAF) Accelerometer, 959 approval of, 576 "Access to Space" study, 22, 80, 172 AXAF-I, 653 ACE-Able Engineering, Inc, 857 AXAF-S, 653 Active Cavity Radiometer Irradiance Monitor budgets and funding for, 653–54, 779 (ACRIM), 421, 480 Chandra (AXAF), 576, 579, 652, 655–57, Acuña, Mario H., 940, 945, 953, 956 838–41 Adamson, James C. characteristics, instruments, and experiments, STS-28, 360, 380 654–57, 838–41; Advanced Charged Couple STS-43, 363, 409 Imaging Spectrometer (ACIS), 656, 657, Adrastea, 711 839, 840; High Energy Transmission Grating Advanced Carrier Customer Equipment Support (HETG) spectrometer, 657, 839–40, 841; System, 223 High Resolution Camera (HRC), 656, 657, Advanced Charged Couple Imaging Spectrometer 839, 840; High Resolution Mirror Assembly, (ACIS), 656, 657, 839, 840 654, 656–57; Low Energy Transmission Advanced Communications Technology Satellite Grating (LETG) spectrometer, 657, 839–40; (ACTS), 161, 252, 254, 366, 454 Science Instrument Module (SIM), 657 Advanced Composition Explorer (ACE), 140, deployment of, 579 579, 604–5, 606, 607, 772, 781, 806–9 development of, 652, 653 Advanced Concepts and Technology, Office of objective of, 589, 652–53 (Code C) Advisory Committee on the Future of the U.S. budgets and funding for, 13, 33, 35, 89, 91, 94, Space Program, 204–5, 287, 564 100 Aero Corporation, 894, 897
    [Show full text]
  • Current Space Launch Vehicles Used by The
    Current Space Launch Vehicles Used by the HEET United States S Nathan Daniels April 2014 At present, the United States relies on Russian rocket engines to launch satellites ACT into space. F The U.S. also relies on Russia to transport its astronauts to the International Space Station (as the U.S. Space Shuttle program ended in 2011). Not only does this reliance have direct implications for our launch capabilities, but it also means that we are funding Russian space and missile technology while we could be investing in U.S. based jobs and the defense industrial base. These facts raises national security concerns, as the United States’ relationship with Russia is ever-changing - the situation in Ukraine is a prime example. This paper serves as a brief, but factual overview of active launch vehicles used by the United States. First, are the three vehicles with the payload capability to launch satellites into orbit: the Atlas V, Delta IV, and the Falcon 9. The other active launch vehicles will follow in alphabetical order. www.AmericanSecurityProject.org 1100 New York Avenue, NW Suite 710W Washington, DC AMERICAN SECURITY PROJECT Atlas Launch Vehicle History and the Current Atlas V • Since its debut in 1957 as America’s first operational intercon- tinental ballistic missile (ICBM) designed by the Convair Divi- sion of General Dynamics, the Atlas family of launch vehicles has logged nearly 600 flights. • The missiles saw brief ICBM service, and the last squadron was taken off of operational alert in 1965. • From 1962 to 1963, Atlas boosters launched the first four Ameri- can astronauts to orbit the Earth.
    [Show full text]
  • Launch Services Overview to the Planetary Exploration Decadal Survey Committee
    Launch Services Overview to the Planetary Exploration Decadal Survey Committee November 17, 2009 Bill Wrobel NASA / SOMD Agenda • Overview • Manifest • Launch Vehicles • Issues 2 Overview • NASA’s Launch Services Program (LSP) was consolidated at KSC in 1998 – LSP provides acquisition, technical management, mission integration and launch management • NASA utilizes a mixed fleet of vehicles (small, medium & intermediate) with varying levels of performance used to support a mix of mission sizes – Mainly for Science Mission Directorate payloads, but SOMD (TDRS) and other government agencies also use NASA launch services – Launches conducted from multiple ranges; CCAFS, VAFB, RTS, WFF, and Kodiak • Vehicles are selected from the NASA Launch Services Contract (NLS) – Through competition based on mass, orbit, class of payload, and best value – Current NLS contract expires in 2010, RFP released to extend the contract • Most recent contract action purchased four intermediate class missions – TDRS – K & L, RBSP and MMS • Important issues – Loss of Medium Class launch service provider, which has been 50% of NASA missions historically – Compressed manifest – Possibility that NASA incurs a portion of the intermediate class infrastructure costs post 2010 3 Launch Services Program Roles & Responsibilities • Identify & Aggregate NASA Space Launch Requirements • Provide Launch Services for Other Agencies, Upon Request • Procure Commercially Available Expendable Launch Vehicle Launch Services to meet Spacecraft mission requirements • Overall Integration
    [Show full text]