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AERONET Annual Review
AERONET Annual Review Colleagues, your AERONET sun and sky scanning network has continued to be a valued resource for basic aerosol research, satellite validation, global and regional aerosol model validation and synergism with field campaigns, in situ and RS observations. Following is my tome on our current state, issues we are facing and plans for the future. 1.0 Introduction and News 2.0 Calibration 3.0 Issues 4.0 Future Developments 5.0 Related Initiatives **Note** Wayne Newcomb, our good friend and primary person responsible for keeping instruments functional network wide and maintaining the swapout rotation through the system among many other things, has made progress in his battle with cancer. After two weeks on life support and multiple surgeries, he’s breathing on his own, talking and is annoyed that he wasn’t able to vote. We’re encouraged by his determination and strength. We need everyone’s help to fill the void left by his absence. We especially need everyone’s support to keep their equipment running in the field. Please see the proactive site manager section under ‘3.0 Issues’. 1.0 Introduction and News I’m very happy to announce the third AERONET workshop and conference to be held in mid August 2009 at or near Hangzhou, China. Although the details will be forthcoming in the months ahead, the plan is for a combined technical and training forum and aerosol science conference that will emphasize surface, airborne and satellite research with several themes. Our host and organizer will be Prof. Jiang Hong of Zhejiang Forestry University and facilitated by Prof. -
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. -
ESPA Ring Datasheet
PAYLOAD ADAPTERS | ESPA ESPA THE EVOLVED SECONDARY PAYLOAD ADAPTER ESPA mounts to the standard NSSL (formerly EELV) interface bolt pattern (Atlas V, Falcon 9, Delta IV, OmegA, Vulcan, Courtesy of Lockheed Martin New Glenn) and is a drop-in component in the launch stack. Small payloads mount to ESPA ports featuring either a Ø15-inch bolt circle with 24 fasteners or a 4-point mount with pads at each corner of a 15-inch square; both of these interfaces have become small satellite standards. ESPA is qualified to carry 567 lbs (257 kg), and a Heavy interface Courtesy of NASA (with Ø5/16” fastener hardware) has been introduced with a capacity of 991 lbs (450 kg). All small satellite mass capabilities require the center of gravity (CG) to be within 20 inches (50.8 cm) of the ESPA port surface. Alternative configurations can be accommodated. ESPA GRANDE ESPA Grande is a more capable version of ESPA with Ø24-inch ports; the ring height is typically 42 inches. The Ø24-inch port has been qualified by test to Courtesy of ORBCOMM & Sierra Nevada Corp. carry small satellites up to 1543 lb (700 kg). ESPA ESPA IS ADAPTABLE TO UNIQUE MISSION REQUIREMENTS • The Air Force’s STP-1 mission delivered multiple small satellites on an Atlas V. • NASA’s Lunar Crater Observation and Sensing Satellite (LCROSS): ESPA was the spacecraft hub for the LCROSS shepherding satellite in 2009. • ORBCOMM Generation 2 (OG2) launched stacks of two and three ESPA Grandes on two different Falcon 9 missions and in total deployed 17 satellites. -
Spaceflight, Inc. General Payload Users Guide
Spaceflight, Inc. SF‐2100‐PUG‐00001 Rev F 2015‐22‐15 Payload Users Guide Spaceflight, Inc. General Payload Users Guide 3415 S. 116th St, Suite 123 Tukwila, WA 98168 866.204.1707 spaceflightindustries.com i Spaceflight, Inc. SF‐2100‐PUG‐00001 Rev F 2015‐22‐15 Payload Users Guide Document Revision History Rev Approval Changes ECN No. Sections / Approved Pages CM Date A 2011‐09‐16 Initial Release Updated electrical interfaces and launch B 2012‐03‐30 environments C 2012‐07‐18 Official release Updated electrical interfaces and launch D 2013‐03‐05 environments, reformatted, and added to sections Updated organization and formatting, E 2014‐04‐15 added content on SHERPA, Mini‐SHERPA and ISS launches, updated RPA CG F 2015‐05‐22 Overall update ii Spaceflight, Inc. SF‐2100‐PUG‐00001 Rev F 2015‐22‐15 Payload Users Guide Table of Contents 1 Introduction ........................................................................................................................... 7 1.1 Document Overview ........................................................................................................................ 7 1.2 Spaceflight Overview ....................................................................................................................... 7 1.3 Hardware Overview ......................................................................................................................... 9 1.4 Mission Management Overview .................................................................................................... 10 2 Secondary -
Commercial Orbital Transportation Services
National Aeronautics and Space Administration Commercial Orbital Transportation Services A New Era in Spaceflight NASA/SP-2014-617 Commercial Orbital Transportation Services A New Era in Spaceflight On the cover: Background photo: The terminator—the line separating the sunlit side of Earth from the side in darkness—marks the changeover between day and night on the ground. By establishing government-industry partnerships, the Commercial Orbital Transportation Services (COTS) program marked a change from the traditional way NASA had worked. Inset photos, right: The COTS program supported two U.S. companies in their efforts to design and build transportation systems to carry cargo to low-Earth orbit. (Top photo—Credit: SpaceX) SpaceX launched its Falcon 9 rocket on May 22, 2012, from Cape Canaveral, Florida. (Second photo) Three days later, the company successfully completed the mission that sent its Dragon spacecraft to the Station. (Third photo—Credit: NASA/Bill Ingalls) Orbital Sciences Corp. sent its Antares rocket on its test flight on April 21, 2013, from a new launchpad on Virginia’s eastern shore. Later that year, the second Antares lifted off with Orbital’s cargo capsule, (Fourth photo) the Cygnus, that berthed with the ISS on September 29, 2013. Both companies successfully proved the capability to deliver cargo to the International Space Station by U.S. commercial companies and began a new era of spaceflight. ISS photo, center left: Benefiting from the success of the partnerships is the International Space Station, pictured as seen by the last Space Shuttle crew that visited the orbiting laboratory (July 19, 2011). More photos of the ISS are featured on the first pages of each chapter. -
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. -
Jacques Tiziou Space Collection
Jacques Tiziou Space Collection Isaac Middleton and Melissa A. N. Keiser 2019 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Biographical / Historical.................................................................................................... 1 Scope and Contents........................................................................................................ 2 Arrangement..................................................................................................................... 2 Names and Subjects ...................................................................................................... 2 Container Listing ............................................................................................................. 4 Series : Files, (bulk 1960-2011)............................................................................... 4 Series : Photography, (bulk 1960-2011)................................................................. 25 Jacques Tiziou Space Collection NASM.2018.0078 Collection Overview Repository: National Air and Space Museum Archives Title: Jacques Tiziou Space Collection Identifier: NASM.2018.0078 Date: (bulk 1960s through -
National Reconnaissance Office Review and Redaction Guide
NRO Approved for Release 16 Dec 2010 —Tep-nm.T7ymqtmthitmemf- (u) National Reconnaissance Office Review and Redaction Guide For Automatic Declassification Of 25-Year-Old Information Version 1.0 2008 Edition Approved: Scott F. Large Director DECL ON: 25x1, 20590201 DRV FROM: NRO Classification Guide 6.0, 20 May 2005 NRO Approved for Release 16 Dec 2010 (U) Table of Contents (U) Preface (U) Background 1 (U) General Methodology 2 (U) File Series Exemptions 4 (U) Continued Exemption from Declassification 4 1. (U) Reveal Information that Involves the Application of Intelligence Sources and Methods (25X1) 6 1.1 (U) Document Administration 7 1.2 (U) About the National Reconnaissance Program (NRP) 10 1.2.1 (U) Fact of Satellite Reconnaissance 10 1.2.2 (U) National Reconnaissance Program Information 12 1.2.3 (U) Organizational Relationships 16 1.2.3.1. (U) SAF/SS 16 1.2.3.2. (U) SAF/SP (Program A) 18 1.2.3.3. (U) CIA (Program B) 18 1.2.3.4. (U) Navy (Program C) 19 1.2.3.5. (U) CIA/Air Force (Program D) 19 1.2.3.6. (U) Defense Recon Support Program (DRSP/DSRP) 19 1.3 (U) Satellite Imagery (IMINT) Systems 21 1.3.1 (U) Imagery System Information 21 1.3.2 (U) Non-Operational IMINT Systems 25 1.3.3 (U) Current and Future IMINT Operational Systems 32 1.3.4 (U) Meteorological Forecasting 33 1.3.5 (U) IMINT System Ground Operations 34 1.4 (U) Signals Intelligence (SIGINT) Systems 36 1.4.1 (U) Signals Intelligence System Information 36 1.4.2 (U) Non-Operational SIGINT Systems 38 1.4.3 (U) Current and Future SIGINT Operational Systems 40 1.4.4 (U) SIGINT -
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......................................... -
Small Satellite Access to ESPA Standard Service
SSC10-IX-1 Small Satellite Access to ESPA Standard Service Mr. Ted Marrujo DoD Space Test Program (STP), Mission Design 3548 Aberdeen Ave. SE, Kirtland AFB NM 87117; (505) 853-3338 Ted. [email protected] Lt Jake Mathis Space and Missile Systems Center, Launch and Range Systems Wing, Engineering 483 N. Aviation Blvd, Los Angeles AFB, CA; (310) 653-3392 [email protected] Mr. Caleb C. Weiss United Launch Alliance, Mission Integration 12257 S. Wadsworth Blvd, TSB-B7140, Littleton, CO 80125; (303) 977-0843 [email protected] ABSTRACT The DoD Space Test Program (STP), the Air Force Launch and Range Systems Wing (LRSW), and United Launch Alliance (ULA) are teaming up to provide a rideshare service to small satellites (<400lb) using an Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter (ESPA). This rideshare service is an opportunity on EELV missions with margin to carry auxiliary payloads (APLs). This paper will define the ESPA, the standard rideshare service provided to APLs, and how APLs can access this service. We will discuss the roles and responsibilities the different government organizations, ULA, and the small satellite provider have in accessing and implementing ESPA Standard Service. In brief, ULA builds the EELV and performs the launch service, LRSW is responsible for developing and acquiring EELVs from ULA, and STP is responsible for identifying and manifesting APLs that meet ESPA Standard Service requirements. We will further define the processes and procedures required to implement ESPA Standard Service to include: how a particular EELV mission is selected to host ESPA Standard Service, the selection process for auxiliary satellites to utilize the capability, the requirements and timelines small satellites must meet to qualify, and the scope of services provided by ULA as part of Standard Service. -
Solar Radiation (SOLRAD) Satellite Summary Table As of 26 March 2004
Solar Radiation (SOLRAD) Satellite Summary Table as of 26 March 2004 Satellite Name Launch Date Transmitter(s) Vanguard 3 18 September 1959 108.00 Mc/s 30 mW FM/PM IRIG 2, 3, 4 & 5 Explorer 7 13 October 1959 19.9915 Mc/s 660 mW FM/AM IRIG 2, 3, 4 & 5 Solrad Dummy 13 April 1960 Inert Test Article Sun Ray 1 22 June 1960 108.00 Mc/s 40 mW FM/AM IRIG Ch 4 & Ch 5 Sun Ray 2 30 November 1960 (Failure) 108.00 Mc/s 40 mW FM/AM IRIG Ch 4 & Ch 5 here Sun Ray 3 29 June 1961 (Partial failure) 108.00 Mc/s Sun Ray 4 24 January 1962 (Failure) 108.09 Mc/s 100 mW FM/AM Sun Ray 4B 26 April 1962 (Failure) 108.00 Mc/s 100 mW FM/AM 20 inch sp Sun Ray 5 Not Launched Sun Ray 6 15 June 1963 136.890 MHz 100 mW FM/AM SolRad 7A 11 January 1964 136.887 MHz 100 mW FM/AM IRIG Ch 3 to 8 SolRad 7B 9 March 1965 136.800 MHz 100 mW FM/AM IRIG Ch 3 to 8 SolRad 8 19 November 1965 137.41 MHz 1W Stored data playback Explorer 30 136.44 MHz 100mW 24 inch sphere Solar Explorer A 136.53 MHz 100mW SolRad 9 5 March 1968 136.41 MHz 500 mW Stored data playback Explorer 37 136.52 MHz 150 mW Primary RT FM/AM IRIG 3 to 8 Solar Explorer B 137.59 MHz 150 mW RT FM/AM IRIG 3 to 7, 12 PCM SolRad 10 8 July 1971 136.38 MHz 250 mW 5W on cmd TM2 - PCM/PM or Stored Data or Stellrad on cmd Explorer 44 137.71 MHz 250 mW TM1 - PAM/PCM/FM/PM RT analog (chs 4-8, COSPAR Ch 7) Solar Explorer-C and digital PCM (ch 12) SolRad 11A & 14 March 1976 137.44 MHz 5W (11A), 136.53 MHz 5W (11B) SolRad 11B 102.4 bps PCM/BiØ-L/PM convolutional encoded (R=½, k=7) Early X-ray missions Name Vanguard 3 Launch Date 1959 September 18.22 UTC SAO ID 1959 ? (Eta) COSPAR ID 1959-07A Catalog No. -
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