The Department of Defense Space Test Program
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Douglas Missile & Space Systems Division
·, THE THOR HISTORY. MAY 1963 DOUGLAS REPORT SM-41860 APPROVED BY: W.H.. HOOPER CHIEF, THOR SYSTEMS ENGINEERING AEROSPACE SYSTEMS ENGINEERING DOUGLAS MISSILE & SPACE SYSTEMS DIVISION ABSTRACT This history is intended as a quick orientation source and as n ready-reference for review of the Thor and its sys tems. The report briefly states the development of Thor, sur'lli-:arizes and chronicles Thor missile and booster launch inGs, provides illustrations and descriptions of the vehicle systcn1s, relates their genealogy, explains sane of the per fon:iance capabilities of the Thor and Thor-based vehicles used, and focuses attention to the exploration of space by Douelas Aircraf't Company, Inc. (DAC). iii PREFACE The purpose of The Thor History is to survey the launch record of the Thor Weapon, Special Weapon, and Space Systems; give a systematic account of the major events; and review Thor's participation in the military and space programs of this nation. The period covered is from December 27, 1955, the date of the first contract award, through May, 1963. V �LE OF CONTENTS Page Contract'Award . • • • • • • • • • • • • • • • • • • • • • • • • • 1 Background • • • • • • • • • • • • • • • • • • • • • • • • • • • • l Basic Or�anization and Objectives • • • • • • • • • • • • • • • • 1 Basic Developmenta� Philosophy . • • • • • • • • • • • • • • • • • 2 Early Research and Development Launches • • • ·• • • • • • • • • • 4 Transition to ICBM with Space Capabilities--Multi-Stage Vehicles . 6 Initial Lunar and Space Probes ••••••• • • • • • • • -
Space) Barriers for 50 Years: the Past, Present, and Future of the Dod Space Test Program
SSC17-X-02 Breaking (Space) Barriers for 50 Years: The Past, Present, and Future of the DoD Space Test Program Barbara Manganis Braun, Sam Myers Sims, James McLeroy The Aerospace Corporation 2155 Louisiana Blvd NE, Suite 5000, Albuquerque, NM 87110-5425; 505-846-8413 [email protected] Colonel Ben Brining USAF SMC/ADS 3548 Aberdeen Ave SE, Kirtland AFB NM 87117-5776; 505-846-8812 [email protected] ABSTRACT 2017 marks the 50th anniversary of the Department of Defense Space Test Program’s (STP) first launch. STP’s predecessor, the Space Experiments Support Program (SESP), launched its first mission in June of 1967; it used a Thor Burner II to launch an Army and a Navy satellite carrying geodesy and aurora experiments. The SESP was renamed to the Space Test Program in July 1971, and has flown over 568 experiments on over 251 missions to date. Today the STP is managed under the Air Force’s Space and Missile Systems Center (SMC) Advanced Systems and Development Directorate (SMC/AD), and continues to provide access to space for DoD-sponsored research and development missions. It relies heavily on small satellites, small launch vehicles, and innovative approaches to space access to perform its mission. INTRODUCTION Today STP continues to provide access to space for DoD-sponsored research and development missions, Since space first became a viable theater of operations relying heavily on small satellites, small launch for the Department of Defense (DoD), space technologies have developed at a rapid rate. Yet while vehicles, and innovative approaches to space access. -
The Advanced Cryogenic Evolved Stage (ACES)- a Low-Cost, Low-Risk Approach to Space Exploration Launch
The Advanced Cryogenic Evolved Stage (ACES)- A Low-Cost, Low-Risk Approach to Space Exploration Launch J. F. LeBar1 and E. C. Cady2 Boeing Phantom Works, Huntington Beach CA 92647 Space exploration top-level objectives have been defined with the United States first returning to the moon as a precursor to missions to Mars and beyond. System architecture studies are being conducted to develop the overall approach and define requirements for the various system elements, both Earth-to-orbit and in-space. One way of minimizing cost and risk is through the use of proven systems and/or multiple-use elements. Use of a Delta IV second stage derivative as a long duration in-space transportation stage offers cost, reliability, and performance advantages over earth-storable propellants and/or all new stages. The Delta IV second stage mission currently is measured in hours, and the various vehicle and propellant systems have been designed for these durations. In order for the ACES to have sufficient life to be useful as an Earth Departure Stage (EDS), many systems must be modified for long duration missions. One of the highest risk subsystems is the propellant storage Thermal Control System (TCS). The ACES effort concentrated on a lower risk passive TCS, the RL10 engine, and the other subsystems. An active TCS incorporating a cryocoolers was also studied. In addition, a number of computational models were developed to aid in the subsystem studies. The high performance TCS developed under ACES was simulated within the Delta IV thermal model and long-duration mission stage performance assessed. -
ULA Rideshare Capabilities for Providing Low-Cost Access to Space
United Launch Alliance Rideshare Capabilities for Providing Low-Cost Access to Space Keith Karuntzos United Launch Alliance PO Box 3788, MIS C4102 Centennial, CO 80155-3788 303-269-5499 [email protected] Abstract-United Launch Alliance (ULA) has a long history of REFERENCES ••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 9 providing launch services to high-value payloads for a variety BIOGRAPHY •••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 9 of customers, including the US Department of Defense, the National Reconnaissance Office, NASA, and commercial customers. These missions have deployed a wide variety of capabilities into Earth orbit and beyond, such as navigation, 1. VVHAT IS RIDESHARE? communication, R&D, observation, and science, all which have Since the dawn of the space age, spacecraft have often provided us with a tremendous amount of knowledge about Earth and our solar system. The majority of these spacecraft shared launch services with one another while being has been launched as primary payloads, and used the full delivered into space. This approach has normally been done capability of the launch vehicle; yet there is a lower-cost to support spacecraftmuch smaller than the primary payload alternative for achieving similar mission objectives: rideshare. it is launching with. By designing launch services in this manner, spacecraft operators were able to deliver more Rideshare is the approach of sharing available launch vehicle payloads to orbit for a fraction of the cost of a full-up launch performance and volume margins with two or more spacecraft service. that would otherwise go underutilized by the spacecraft community. This allows spacecraft customers the opportunity This method of launching multiple payloads into orbit on a to get their spacecraft to orbit and beyond in an inexpensive single launch vehicle is called rideshare. -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 2 May–June 2019 CONTENTS FOCUS ..................................................................................................................... 1 European industrial leadership at stake ............................................................................ 1 SPACE POLICY AND PROGRAMMES .................................................................................... 2 EUROPE ................................................................................................................. 2 9th EU-ESA Space Council .......................................................................................... 2 Europe’s Martian ambitions take shape ......................................................................... 2 ESA’s advancements on Planetary Defence Systems ........................................................... 2 ESA prepares for rescuing Humans on Moon .................................................................... 3 ESA’s private partnerships ......................................................................................... 3 ESA’s international cooperation with Japan .................................................................... 3 New EU Parliament, new EU European Space Policy? ......................................................... 3 France reflects on its competitiveness and defence posture in space ...................................... 3 Germany joins consortium to support a European reusable rocket......................................... -
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. -
1985 Twenty-Second Space Congress Program
Space Congress Programs 4-23-1985 1985 Twenty-Second Space Congress Program Canaveral Council of Technical Societies Follow this and additional works at: https://commons.erau.edu/space-congress-programs Scholarly Commons Citation Canaveral Council of Technical Societies, "1985 Twenty-Second Space Congress Program" (1985). Space Congress Programs. 26. https://commons.erau.edu/space-congress-programs/26 This Book is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Space Congress Programs by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. en c en 2 w a: 0 CJ CJ z w 0 UJ 0 I w > 0 1- <( 2 D.. w en .·;: ' I- Cocoa Beach, Florida April 23, 24, 25, 26, 1985 CHAIRMAN'S MESSAGE The theme of the Twenty Second Space Congress is Space and Society - Pro gress and Promise. This is appropriate for the matu rity of world wide space activities as well as descrip tive of the planned pro gram. Congressman Don Fuqua, Chairman, Committee on Science & Technology will present the keynote address followed by a high level DOD Panel describing multi service space activities. To- day's space program wil l be further discussed in sessions covering Space Shuttle Operational Efficiency, Spacelab Missions, Getaway Specials, and International Space Programs. Society is not only more aware but also becoming directly active in Space through Getaway Specials on Shuttle as well as the advent of major activities to be covered in a panel on Commercialization. Other near term new initiatives are covered in panels on Space Defense Initiative and Space Station Plans & Development. -
Evolved Expendable Launch Operations at Cape Canaveral, 2002-2009
EVOLVED EXPENDABLE LAUNCH OPERATIONS AT CAPE CANAVERAL 2002 – 2009 by Mark C. Cleary 45th SPACE WING History Office PREFACE This study addresses ATLAS V and DELTA IV Evolved Expendable Launch Vehicle (EELV) operations at Cape Canaveral, Florida. It features all the EELV missions launched from the Cape through the end of Calendar Year (CY) 2009. In addition, the first chapter provides an overview of the EELV effort in the 1990s, summaries of EELV contracts and requests for facilities at Cape Canaveral, deactivation and/or reconstruction of launch complexes 37 and 41 to support EELV operations, typical EELV flight profiles, and military supervision of EELV space operations. The lion’s share of this work highlights EELV launch campaigns and the outcome of each flight through the end of 2009. To avoid confusion, ATLAS V missions are presented in Chapter II, and DELTA IV missions appear in Chapter III. Furthermore, missions are placed in three categories within each chapter: 1) commercial, 2) civilian agency, and 3) military space operations. All EELV customers employ commercial launch contractors to put their respective payloads into orbit. Consequently, the type of agency sponsoring a payload (the Air Force, NASA, NOAA or a commercial satellite company) determines where its mission summary is placed. Range officials mark all launch times in Greenwich Mean Time, as indicated by a “Z” at various points in the narrative. Unfortunately, the convention creates a one-day discrepancy between the local date reported by the media and the “Z” time’s date whenever the launch occurs late at night, but before midnight. (This proved true for seven of the military ATLAS V and DELTA IV missions presented here.) In any event, competent authorities have reviewed all the material presented in this study, and it is releasable to the general public. -
Two-Stage, High-Altitude Rocket with Internal Skeleton Design Entered in Advance Category of 7Th ESRA IREC
Two-Stage, High-Altitude Rocket with Internal Skeleton Design Entered in Advance Category of 7th ESRA IREC Samuel S. Bowman1, Kevin J. Byrne2, Allen Capatina3, Aliki S. Loper-Leddy4, and Joshua A. Van Schoyck5 California Polytechnic State University, San Luis Obispo, CA, 93407 A high-altitude, two-stage rocket was designed, built, and entered in the advanced category of the 7th Annual Experimental Sounding Rocket Association (ESRA) Intercollegiate Rocketry Engineering Competition (IREC). The rocket, called AJAKS, featured an internal skeleton made of carbon fiber rods, and a combination of plywood, carbon, and aluminum bulkheads. Loads were driven through the internal structure, with an outer skin tube providing an aerodynamic surface. A unique separation device was developed to ensure proper stage separation. The competition required the rocket to carry a 10-lb payload, which was chosen by the team to consist of an IMU and data logging computer for recording the descent profile, a CubeSat test unit, and a digital video recorder. Prior to the competition launch, AJAKS was test launched on May 5th in the Mojave at the Friends of Amateur Rocketry (FAR) launch facility. During the test launch AJAKS suffered a PIRM malfunction and the main parachute did not deploy. Following the test launch, the second stage of the rocket was rebuilt with a stronger payload configuration. The ESRA IREC was held on June 21st to the 24th. AJAKS was launched on the 23rd and during ascent the second stage became unstable and reached an altitude of only 6,000 ft. Both stages suffered damage upon landing. Nomenclature A = reference area (inches2) CNα = normal force coefficient (unitless) cp = center of pressure location relative to nosecone tip (inches) E = elastic modulus (psi) I = area moment of inertia (inches2) L = length of the rocket (inches) Pcr = critical load for buckling (pounds) Subscripts b = first stage s = second stage total = first and second stage I. -
Hitchhiker on Space Station ISS Hitchhrker STUDY
Hitchhiker On Space Station Gerard Daelemans NASA Goddard Space FlightCenter (301) 286-2193 Theodore Goldsmith Swales Aerospace Inc. (301) 902-4536 ABSTRACT The NASA/GSFC ShuttleSmall PayloadsProjectsOffice(SSPPO) has been studyingthe feasibilityof migrating Hitchhikercustomers pastpresentand futureto the InternationalSpace Stationvia a "Hitchhikerlike"carrier system.SSPPO has been taskedto make themost use of existinghardware and soft-waresystemsand infrastructurein itsstudyof an ISS based carriersystem. This paper summarizes the resultsof the SSPPO Hitchhikeron International Space Station(ISS)study. Includedare a number of"Hitchhikerlike"carrier system conceptsthat take advantage of the various ISS attached payload accommodation sites.Emphasis willbe givento a HI-Iconceptthatattachesto theJapaneseExperimentModule - Exposed Facility(JEM-EF). ISS HITCHHrKER STUDY OBJECTIVES The objectives of the Hitchhiker on ISS study were to examine the potential for using existing or modified Shuttle Hitchhiker flight and ground systems, facilities, personnel, and general low-cost, quick reaction approach to support smaller scientific payloads on Space Station. Any such implementation should avoid duplicating any already planned ISS capabilities and allow for easy transition of existing Shuttle Hitchhiker customers to ISS. EXISTING PLANNED SPACE STATION EXTERNAL PAYLOAD ACCOMMODATIONS Existing plans for Space Station external payload accommodations were examined in detail in order to determine the most promising possibilities for complementary use of Hitchhiker derived systems and implementation approach. The current plans are summarized as follows: The ISS has attachment latches (the Payload Attach System (PAS)) located on the main truss. Two are located on the nominal top (zenith - space facing) side of the starboard ($3) truss and a second pair are located on the bottom (nadir - earth facing) side. An additional set (upper and lower) of latches is located on the port side (P3) of the truss. -
N E W S L E T T
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External Payloads Proposer's Guide to the International Space Station
SSP 51071 Baseline External Payloads Proposer’s Guide to the International Space Station International Space Station Program Baseline August 2017 National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas This Document Is Uncontrolled When Printed. Verify Current version before use. SSP 51071 Baseline REVISION AND HISTORY REV. DESCRIPTION PUB. DATE - Initial Release (Reference per SSCD 15774, EFF. 09-29-2017) 10-02-17 Public access authorization obtained via the Document Availability Authorization Control Number: “40352” This Document Is Uncontrolled When Printed. Verify Current Version Before Use. SSP 51071 Baseline TABLE OF CONTENTS PARAGRAPH PAGE 1.0 INTRODUCTION ................................................................................................................... 1-1 2.0 GENERAL INFORMATION FOR OPERATING ON ISS ........................................................ 2-1 2.1 HOW TO GET STARTED ...................................................................................................... 2-1 2.2 ISS FEASIBILITY RESOURCE ACCOMMODATION ASSESSMENT PROCESS ................ 2-2 2.3 WHAT YOU SHOULD KNOW ............................................................................................... 2-5 2.4 ORGANIZATIONAL ROLES/RESPONSIBILITIES ................................................................ 2-7 2.5 ROLES/RESPONSIBILITIES OF PAYLOAD PROVIDERS ................................................... 2-8 3.0 COMMON ACCOMMODATIONS, RESOURCES, AND ENVIRONMENTS