Relative Navigation Light Detection and Ranging (LIDAR) Sensor Development Test Objective (DTO) Performance Verification
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Lighting up to 7 Times Brighter Than Other LED Landing Lights!
Lighting FAA-PMA Approved AeroLEDs Lighting Increase safety and reduce operating cost! See the Difference... Lighting Know the Difference... • Increased safety • Direct replacement • Up to 80% reduced power consumption • Long life - over 50,000 hours! • Lighter weight - no heavy power supply - save up to 3 lbs • Reduced drag • Zero maintenance • 10x more efficient than incandescent! Increased Safety AeroLED lights allow you to comply with the latest FAA recommendations (Operation Lights On) regarding extended use of taxi, landing, and anti-collision lights without fear of reduced light performance or life. They all feature optimized light color (6500k sunlight equivalent) for proven superior air-to-air recognition. The landing and taxi lights also feature an optional pulsed recognition light mode. Reduced Power Consumption High efficiency LED lights use less than 1/3 the power of halogen bulbs. They significantly reduce the load on the electrical system and they won't dim due to low voltage, typical of low RPM final approaches when you need them most! Postition lights aerodynamic design results in less drag than original equipment! Longer Life - Zero Maintenance All AeroLED products are designed to be a "lifetime buy". They last over 50,000 hours when properly installed and do not degrade with on/off cycles. They are extremely rugged and hardened against all kinds of electrical damage, shock, and vibration. Up to 7 times brighter than other LED landing lights! PAR36 Landing Light Comparison Measured Brightness at 50 Ft. Manufacturer Intensity -
STS-135: the Final Mission Dedicated to the Courageous Men and Women Who Have Devoted Their Lives to the Space Shuttle Program and the Pursuit of Space Exploration
National Aeronautics and Space Administration STS-135: The Final Mission Dedicated to the courageous men and women who have devoted their lives to the Space Shuttle Program and the pursuit of space exploration PRESS KIT/JULY 2011 www.nasa.gov 2 011 2009 2008 2007 2003 2002 2001 1999 1998 1996 1994 1992 1991 1990 1989 STS-1: The First Mission 1985 1981 CONTENTS Section Page SPACE SHUTTLE HISTORY ...................................................................................................... 1 INTRODUCTION ................................................................................................................................... 1 SPACE SHUTTLE CONCEPT AND DEVELOPMENT ................................................................................... 2 THE SPACE SHUTTLE ERA BEGINS ....................................................................................................... 7 NASA REBOUNDS INTO SPACE ............................................................................................................ 14 FROM MIR TO THE INTERNATIONAL SPACE STATION .......................................................................... 20 STATION ASSEMBLY COMPLETED AFTER COLUMBIA ........................................................................... 25 MISSION CONTROL ROSES EXPRESS THANKS, SUPPORT .................................................................... 30 SPACE SHUTTLE PROGRAM’S KEY STATISTICS (THRU STS-134) ........................................................ 32 THE ORBITER FLEET ............................................................................................................................ -
Navstrobe Lighting – Kuntzleman
NAVSTROBE LIGHTING – KUNTZLEMAN AIRCRAFT SEXTANT NAV NAVSTROBE PAR 36 LED SYSTEM WITH CONSTANT + LANDING LIGHT CM FAST STROBE 40W Aircraft PAR36 Landing Light, 220w, 109, 400 LM These bulbs are standard parts and have been LEDs. designed to meet the requirements of TSO-C30c. These are non-TSO’d Complete combination navigation and strobe lights P/N 11-14745 .........$209.95 for your aircraft. Emitter Types: Cree LED’s. Turn on first: Constant lighting / Turn on second time <3s: WP Fast Strobe. Switch between modes in fog/cloud etc. P/N 11-14934 .........$429.00 NAVSTROBE PAR 36 LED TAXI LIGHT NAVSTROBE AIRCRAFT Aircraft PAR36 Taxi Light, 220w, 109, 400 LM LEDs. NAVIGATION SYSTEM These are non-TSO’d ME 2 Modes: Constant & Fast Strobe. P/N 11-14744 .........$221.95 Kit Includes: • 2ea. Wingtip combination navigation and strobe light (BAY15scs-10w-A-1512) • 1ea. White tailfin combination navigation and strobe light BEACON LIGHT CONSTANT (BA15sWcs-10w-1156) • 2ea. Lens cover gaskets (Sextant A450) • 1ea. Dielectric grease pouch & FAST WHITE STROBES HA (Sextant 31880) ...........P/N 11-16470 .........$166.80 Note: For Experimental aircraft use only. Not FAA/ PMA Approved. NavStrobe Aircraft Beacon Light AIRCRAFT ANTI- with Constant & Fast White Strobe 503 LM LED’s. Dimensions: 1.9 in x 0.7 in (49.0 mm x 1.8 cm) COLLISION STROBE LIGHT Weight: 0.32 oz (9 g). 10-28VDC. Aircraft Anti-Collision Strobe Light, 45w, Turn on first: Constant lighting / Turn on second time <3s: Fast Strobe. 1350 LM CREE LEDs. Total Emitters: 9 x AP Switch between modes in fog/cloud etc. -
Batonomous Moon Cave Explorer) Mission
DEGREE PROJECT IN VEHICLE ENGINEERING, SECOND CYCLE, 30 CREDITS STOCKHOLM, SWEDEN 2019 Analysis and Definition of the BAT- ME (BATonomous Moon cave Explorer) Mission Analys och bestämning av BAT-ME (BATonomous Moon cave Explorer) missionen ALEXANDRU CAMIL MURESAN KTH ROYAL INSTITUTE OF TECHNOLOGY SCHOOL OF ENGINEERING SCIENCES Analysis and Definition of the BAT-ME (BATonomous Moon cave Explorer) Mission In Collaboration with Alexandru Camil Muresan KTH Supervisor: Christer Fuglesang Industrial Supervisor: Pau Mallol Master of Science Thesis, Aerospace Engineering, Department of Vehicle Engineering, KTH KTH ROYAL INSTITUTE OF TECHNOLOGY Abstract Humanity has always wanted to explore the world we live in and answer different questions about our universe. After the International Space Station will end its service one possible next step could be a Moon Outpost: a convenient location for research, astronaut training and technological development that would enable long-duration space. This location can be inside one of the presumed lava tubes that should be present under the surface but would first need to be inspected, possibly by machine capable of capturing and relaying a map to a team on Earth. In this report the past and future Moon base missions will be summarized considering feasible outpost scenarios from the space companies or agencies. and their prospected manned budget. Potential mission profiles, objectives, requirements and constrains of the BATonomous Moon cave Explorer (BAT- ME) mission will be discussed and defined. Vehicle and mission concept will be addressed, comparing and presenting possible propulsion or locomotion approaches inside the lava tube. The Inkonova “Batonomous™” system is capable of providing Simultaneous Localization And Mapping (SLAM), relay the created maps, with the possibility to easily integrate the system on any kind of vehicle that would function in a real-life scenario. -
International Space Station Benefits for Humanity, 3Rd Edition
International Space Station Benefits for Humanity 3RD Edition This book was developed collaboratively by the members of the International Space Station (ISS) Program Science Forum (PSF), which includes the National Aeronautics and Space Administration (NASA), Canadian Space Agency (CSA), European Space Agency (ESA), Japan Aerospace Exploration Agency (JAXA), State Space Corporation ROSCOSMOS (ROSCOSMOS), and the Italian Space Agency (ASI). NP-2018-06-013-JSC i Acknowledgments A Product of the International Space Station Program Science Forum National Aeronautics and Space Administration: Executive Editors: Julie Robinson, Kirt Costello, Pete Hasbrook, Julie Robinson David Brady, Tara Ruttley, Bryan Dansberry, Kirt Costello William Stefanov, Shoyeb ‘Sunny’ Panjwani, Managing Editor: Alex Macdonald, Michael Read, Ousmane Diallo, David Brady Tracy Thumm, Jenny Howard, Melissa Gaskill, Judy Tate-Brown Section Editors: Tara Ruttley Canadian Space Agency: Bryan Dansberry Luchino Cohen, Isabelle Marcil, Sara Millington-Veloza, William Stefanov David Haight, Louise Beauchamp Tracy Parr-Thumm European Space Agency: Michael Read Andreas Schoen, Jennifer Ngo-Anh, Jon Weems, Cover Designer: Eric Istasse, Jason Hatton, Stefaan De Mey Erik Lopez Japan Aerospace Exploration Agency: Technical Editor: Masaki Shirakawa, Kazuo Umezawa, Sakiko Kamesaki, Susan Breeden Sayaka Umemura, Yoko Kitami Graphic Designer: State Space Corporation ROSCOSMOS: Cynthia Bush Georgy Karabadzhak, Vasily Savinkov, Elena Lavrenko, Igor Sorokin, Natalya Zhukova, Natalia Biryukova, -
L-382J Rev 1
U.S. Department of Transportation Federal Aviation Administration Washington, DC Master Minimum Equipment List (MMEL) Revision: 1 Date: 07/21/2017 L-382J Lockheed Michael Nash, Chair Flight Operations Evaluation Board (FOEB) Federal Aviation Administration (FAA) Long Beach Aircraft Evaluation Group (LGB-AEG) 3960 Paramount Blvd., Suite 100 Lakewood, CA 90712-4137 Telephone: (562) 627-5270 Fax: (562) 627-5281 U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. L-382J DATE: 07/21/2017 I TABLE OF CONTENTS AND CONTROL PAGE SYSTEM NO. SYSTEM PAGE NO. REV NO. DATE -- Cover Page -- 1 07/21/2017 -- Table of Contents and Control Page I 1 07/21/2017 -- Log of Revisions II 1 07/21/2017 -- Highlights of Change III 1 07/21/2017 -- Definitions IV 1 07/21/2017 -- Preamble V 1 07/21/2017 -- Guidelines for (M) and (O) Procedures VI 1 07/21/2017 21 Air Conditioning 21-1 thru 3 1 07/21/2017 22 Autoflight 22-1 thru 5 1 07/21/2017 23 Communications 23-1 thru 3 1 07/21/2017 24 Electrical Power 24-1 thru 2 1 07/21/2017 25 Equipment/Furnishings 25-1 thru 7 1 07/21/2017 26 Fire Protection 26-1 thru 2 1 07/21/2017 27 Flight Controls 27-1 1 07/21/2017 28 Fuel 28-1 thru 6 1 07/21/2017 29 Hydraulic Power 29-1 1 07/21/2017 30 Ice and Rain Protection 30-1 thru 3 1 07/21/2017 31 Indicating/Recording Systems 31-1 thru 3 1 07/21/2017 32 Landing Gear 32-1 1 07/21/2017 33 Lights 33-1 thru 4 1 07/21/2017 34 Navigation 34-1 thru 7 1 07/21/2017 35 Oxygen 35-1 1 07/21/2017 36 Pneumatic 36-1 1 07/21/2017 38 Water/Waste 38-1 1 07/21/2017 45 Central Maintenance System 45-1 1 07/21/2017 46 System Integration and Display 46-1 thru 4 1 07/21/2017 48 Communication/Navigation 48-1 1 07/21/2017 Identification 49 Airborne Auxiliary Power 49-1 1 07/21/2017 52 Doors 52-1 1 07/21/2017 61 Propellers 61-1 1 07/21/2017 73 Engine Fuel and Control 73-1 1 07/21/2017 77 Engine Indicating 77-1 1 07/21/2017 79 Engine Oil 79-1 1 07/21/2017 U.S. -
Lighting Honeywell
HONEYWELL Lighting Aircraft Support Stocking Distributor Honeywell Aerospace is a leading global provider of various Aircraft Lighting systems of both military and civilian aircraft. AllClear is Honeywell’s Worldwide Sole Stocking Distributor for Military Aircraft Fixed and Rotary Wing Lighting. Aircraft Support Stocking Distributor Honeywell Aerospace is a leading global provider of various Aircraft Lighting systems of both military and civilian aircraft. AllClear is Honeywell’s Worldwide Sole Stocking Distributor for Military Aircraft Fixed and Rotary Wing Lighting. • Search Lights • Dome Lights Honeywell• Instrumental Lights • Transformers • Navigational Lights • Power Supplies Aircraft support• Landing stocking Lights distributor• Lenses Aircraft Support Stocking Distributor Honeywell Aerospace• Recognition is a leading Lights global •provider Light Panels of Honeywell Aerospace is a leading global provider of various Aircraft Lighting various Aircraft •Lighting Warning systemsLights of both •military Switches and systems of both military and civilian aircraft. AllClear is Honeywell’s Worldwide civilian aircraft. AllClear is Honeywell’s worldwide sole stocking distributor• Cockpit for military Lights aircraft fixed• Blowers, and rotary Fans Sole Stocking Distributor for Military Aircraft Fixed and Rotary Wing Lighting. wing lighting. • Flood• Search Lights Lights • DC• DomeMotors Lights • Instrumental Lights • Transformers • Navigational Lights • Power Supplies Aircraft Support Stocking Distributor • Landing Lights • Lenses Honeywell Aerospace is a leading global provider of various Aircraft Lighting • Recognition Lights • Light Panels systems of both military and civilian aircraft. AllClear is Honeywell’s Worldwide •Search Lights • Warning Lights • Switches Sole Stocking Distributor for Military Aircraft Fixed and Rotary Wing Lighting. •Instrumental Lights• Cockpit Lights • Blowers, Fans Copyright © 1993 - 2020 AllClear Rev.2020.08.01 • Flood Lights • DC Motors 2525 Collier Canyon Rd. -
A Survey of LIDAR Technology and Its Use in Spacecraft Relative Navigation
https://ntrs.nasa.gov/search.jsp?R=20140000616 2019-08-29T15:23:06+00:00Z CORE Metadata, citation and similar papers at core.ac.uk Provided by NASA Technical Reports Server A Survey of LIDAR Technology and its Use in Spacecraft Relative Navigation John A. Christian* West Virginia University, Morgantown, WV 26506 Scott Cryan† NASA Johnson Space Center, Houston, TX 77058 This paper provides a survey of modern LIght Detection And Ranging (LIDAR) sensors from a perspective of how they can be used for spacecraft relative navigation. In addition to LIDAR technology commonly used in space applications today (e.g. scanning, flash), this paper reviews emerging LIDAR technologies gaining traction in other non-aerospace fields. The discussion will include an overview of sensor operating principles and specific pros/cons for each type of LIDAR. This paper provides a comprehensive review of LIDAR technology as applied specifically to spacecraft relative navigation. I. Introduction HE problem of orbital rendezvous and docking has been a consistent challenge for complex space missions T since before the Gemini 8 spacecraft performed the first successful on-orbit docking of two spacecraft in 1966. Over the years, a great deal of effort has been devoted to advancing technology associated with all aspects of the rendezvous, proximity operations, and docking (RPOD) flight phase. After years of perfecting the art of crewed rendezvous with the Gemini, Apollo, and Space Shuttle programs, NASA began investigating the problem of autonomous rendezvous and docking (AR&D) to support a host of different mission applications. Some of these applications include autonomous resupply of the International Space Station (ISS), robotic servicing/refueling of existing orbital assets, and on-orbit assembly.1 The push towards a robust AR&D capability has led to an intensified interest in a number of different sensors capable of providing insight into the relative state of two spacecraft. -
GENERAL the Lighting System Provides Interior and Exterior
Bombardier Challenger 605 - Lighting GENERAL The lighting system provides interior and exterior illumination of the aircraft. In addition, lights provide information and guidance to passengers in normal and emergency situations. The lighting system includes: • Exterior lighting; • Flight compartment lighting; • Passenger compartment (cabin) lighting; • Service lighting; and • Emergency lighting. EXTERIOR LIGHTING Description The exterior lighting system is controlled from the EXTERNAL LTS panel or the LANDING LTS panel, and consists of the following: • Navigation lights; • Beacon light; • Anti-collision lights; • Logo lights; • Wing inspection lights; • Landing lights; and • Recognition/taxi lights. Components and Operation Navigation Lights The navigation lights are located in each wing tip, fuselage tail cone tip, and at the tip of the stabilizer fairing. A wing tip assembly contains two navigation lights that work simultaneously. Wing Tip Navigation Light Figure 16−10−1 The NAV switch controls the navigation lights (see Figure 16−10−2). Page 1 Bombardier Challenger 605 - Lighting EXTERIOR LIGHTING (CONT'D) Beacon Light There are two red beacon lights located on the top and bottom of the fuselage, near the middle of the aircraft. The BEACON switch controls the beacon lights (see Figure 16−10−3). Anticollision Lights The anticollision lights consist of two wing tip strobe lights, located in the wing tip assembly, and one strobe light at the tip of the fuselage tail cone, co-located with the navigation light. The A/COLL switch controls the anticollision strobe lights (see Figure 16−10−3). Logo Lights The logo lights are located on top of the aircraft’s engine pylons. When selected, these lights illuminate the aircraft’s vertical stabilizer. -
C-5 Handbook
FOR TRAINING USE ONLY C-5 HANDBOOK FOR TRAINING USE ONLY INTRODUCTION This book is designed to be used as a T.O. title. Example: page 3-1 comes from quick-reference pocket handbook T.O. 1C-5A-2-3/Pneudraulics. describing the systems and subsystems of the C-5 Galaxy aircraft. Basically, the handbook consists of descriptive text relating to pictures or As a training aid, this book gives you the drawings of the airplanes structural and distinct advantage of having the general system components. information of twelve aircraft T.O.s condensed into one handbook. For the most part, pictures and text within the book reflect that of the C-5B model The book is formatted in accordance with aircraft. However, in some cases, the aircraft T.O.s, 1C-5A-2-1 through references to "A-model not modified" and 2-13, with the exception of the 2-11 wiring AF68-213 and AF68-216 "Space diagrams, which, due to the size and Container Module (SCM) airplanes " have content could not be included. Each been included. chapter in the handbook represents an aircraft T.O. starting with the 2-1. ALTHOUGH THIS HANDBOOK IS Additionally, for quick reference DERIVED FROM TECH DATA, IT IS purposes, the first digit of the page NOT INTENDED TO REPLACE THE numbers represents the last number of T.O.s. NOR, WILL IT BE USED AS the T.O. from which the information was SUCH. obtained and the page header reflects the i PRESSURES, READINGS, AND LIMITATIONS ARE SUBJECT TO CHANGE AND ARE ONLY USED IN THIS BOOK TO PROVIDE GENERAL PARAMETERS ii TABLE OF CONTENTS INTRODUCTION . -
What Navigation Lights Do I Need
® NAVIGATION LIGHTS Navigation Lights Disclaimer: This information is correct as “A set of lights shown by a ship or aircraft between sunset and at 1st November 2016, and is sunrise, and in rain and fog, to indicate its position and orientation.” designed as a basic guide and RAILBLAZA illuminate Series Battery Powered Navigation introduction to navigation Lights are designed primarily to meet the US Coast Guard requirements lighting for water craft. It is (USCG 2NM) for navigation lights on power boats under 12 metres (39.4’) not to be used as a technical in length. They are made in New Zealand, from high quality materials, and reference. RAILBLAZA assume no deliver fantastic performance at an affordable price. responsibility for any errors or omissions. Please check with the Requirements for vessels under 12 metres appropriate governing body regarding full regulations for navigation All vessels under 12 metres shall exhibit one of the following: lights in your area. • Separate or combined sidelights; a masthead light and a stern light • Separate or combined sidelights and an all round white light. Some internet references for your local region; The masthead or white all round light shall be carried at least one metre New Zealand above the sidelights. http://www.maritimenz.govt.nz/recreational/documents/Safer-Boating- an-essential-guide-2014.pdf Power-driven vessels less than 7 meters in length whose maximum Australia: speed does not exceed 7 knots may in lieu of the above exhibit an all- • QLD http://www.msq.qld.gov.au/Safety/Navigation-lights round white light and shall, if practicable, also exhibit sidelights • NSW http://www.rms.nsw.gov.au/maritime/safety-rules/rules- Form and Function of RAILBLAZA Lights regulations/night-safety.html There are two models in the illuminate Series, the i360 All-round white, • TAS http://www.mast.tas.gov.au/recreational/navigation/ and the iPS Port/Starboard. -
Specifications
SPECIFICATIONS OFFICIAL NO 1147419 LENGTH 50FT BREADTH 15.0 FT GROSS TONNAGE 33 SPEED 28 MPH PASSENGERS 25 FUEL 500 DECK SPACE 16X10 DESCRIPTION: Vessel was built of all welded aluminum construction by owner in Chauvin, La during 2004. Vessel has a flush deck, model bow, square stern and aluminum superstructure with aluminum watertight doors and rubber gasket mounted weather tight windows This vessel is a typical coastal crew boat with a hard chine and a vee'd bottom. The construction is a typical all aluminum crew boat utilized in the oil industry. This vessel has been updated and repowered in July of 2011 HULL CONSTRUCTION Bottom plating is 1/4" original thickness except for last 20ft which is 3/8" aluminum plate. Side plating is 1/4" original thickness. Vessel is framed both longitudinally and transversely with aluminum bulbous tees. FENDER SYSTEM Hull is fitted with the following fender system. Upper strake is located at the weather deck elevation and extends from bow to stern. Second strake is located approximately 18' below and extends from stern forward approximately 20". Fender system is constructed of approximately 2-1/2" split aluminum pipe. Fender system is installed on each side. In addition, vessel is fitted with heavy tires installed on each side from the pilothouse aft to the stern on each side. BULWARKS Bulwarks are non-existent; however vessel is fitted with an approximate 12" high toe rail, installed from the bow stem aft approximately 10" on each port and starboard side DECK FITTINGS Deck fittings are located as follows; located on the bow on centerline, is one (1) approximate 3" diameter single aluminum bit.