Tethered Aerostats & Launch Recovery Systems

Slides:



Advertisements
Similar presentations
Electrical Systems Chapter 9.
Advertisements

Setup/Installation/Operation of an Environmental Control Unit (ECU)
VSE Corporation Proprietary Information
High-Pressure Air Bags 101
ODS3F –Observation and Detection Systems For Forest Fire Monitoring
Unmanned Aerial Vehicles Presentation. Customization for each client Each order is specifically designed to meet each clients’ aerial needs. On-board.
Daniel Graves –Project Lead James Reepmeyer – Lead Engineer Brian Smaszcz– Airframe Design Alex Funiciello – Airfoil Design Michael Hardbarger – Control.
The Load Bank of Choice
Vex 1.0 © 2006 Carnegie Mellon Robotics Academy Inc. Test Bed Assembly.
REAL-TIME SOFTWARE SYSTEMS DEVELOPMENT Instructor: Dr. Hany H. Ammar Dept. of Computer Science and Electrical Engineering, WVU.
PHSAUTOMOTIVESALSPHSAUTOMOTIVESALS Charging System tests & Voltage information Checking the charging system with just a volt meter.
Electrical Power Systems
Sensors and Actuators John Errington MSc. Sensors and Actuators Sensors produce a signal in response to a change in their surroundings e.g. Thermostat.
Network Cabling and Wireless Network
Electro-Pneumatics Module 1
SFC UPSHAW POWER GENERATION EQUIPMENT Preventive Maintenance & Troubleshooting.
EZ Reach 40 Training & Procedure Manual. Unit Capacity One of the most important considerations when operating this machine is the Bucket Capacity of.
Team 4 “Flying Wind Turbine” Jason Landry Bryan MacDonald Scott Montgomerie Daniel Pollock Robert Ringrose Dr. Dale Retallack Team Members Supervisor.
Robert Simon, Coleman Hostetler, Aashay Sukhthankar, Devin Moore.
AEM 5333 UAV Search and Surveillance. Mission Description Overhead surveillance and tracking – Humans on foot – Moving vehicles Onboard GPS transceiver.
MIT ROV TEAM Michelle Aquing, Heather Brundage, Lauren Cooney, Bridget Downey, Eddie Huo, Albert Kwon, Harry Lichter, M. Jordan Stanway, Kurt Stiehl, ThaddeusStefanov-
PROGRAMMABLE LOGIC CONTROLLER (PLC) AND AUTOMATION
Vehicle Characteristics/Pre-Checks/ Driving/Winching
Team SSCSC Critical Design Review Nick Brennan, Kier Fortier, Tom Johnson, Shannon Martin, Dylan Stewart, and Adam Wright October 05, 2010 Fall 2010 Rev.
JLENS The Joint Land Attack Cruise Missile Defense Elevated Netted Sensor System.
Types of Fire Apparatus Equipped with a Fire Pump Sugar Land Fire Department Driver/Operator—Pumper Academy Spring 2003.
URW295C4URS (Tracked, Diesel)SPYDERCRANE Capabilities.
SCADA Supervisory Control And Data Acquisition Pantech Solutions Here is the key to learn more.
AC DC Not the awesome, long-may-they- reign, Australian kings of the power chord ……..
III ALTERNATING CURRENT Electricity is generated, transmitted, and used in the form of three-phase alternating current (AC). The current strength of AC.
CGS Ground School Technical The Vigilant Electrical System © Crown Copyright 2012 No Part of this presentation may be reproduced without the permission.
Generac 5943 GP7500E 7,500 Watt 420cc OHV Portable Gas Powered Generator.
PPT of topic § Electric Cars and Hybrid vehicles - Electric Cars
Gas Turbine Power Plant
Automatic Transfer Switches
Simulation-to-Flight 1 Additional Resources:
CHAPTER 3 Physical Layer.
AC DC Not the awesome, long-may-they-reign, Australian kings of the power chord ……..
Preliminary Design Review
Lighter Than Air Platforms
SkyDoc™ Aerostat and Launch Systems
Single Phase Induction
Power Supply.
HIAB TRANSPORT HIRE SERVICES BY DELTA TRANSPORT
How SCADA Systems Work?.
Connections Topology of Apollo ACS.
8th Grade Weather Balloon TEAM NAME???? LOGO?????? 2016
Trane Standby Generators
Chapter 8 – Cutting Processes
Energy Consumption: HOME.
Circuit Breakers & Reclosers
Energy Consumption: HOME.
Mobile Cellular Communications System
CHAPTER 3 Physical Layer.
Wind Farm: Generators that produce AC are generally equipped with features to produce the correct voltage (120 or 240 V) and constant frequency.
Electric braking Powerpoint presentation by:- Poonam sharma
ELECTRICAL POWER-II Electrical engineering sixth semester
Sizing Methodologies • Sizing Calculations
Shipboard Configurations
Towing Small Utility Trailers
Energy Consumption: HOME.
Screwfox: Manual and Battery Powered Torque Screwdrivers
Unit 2 Unmanned Aircraft
AUTOMOBILE ENGINEERING.
1.11: Robot Controller.
Fiber Optic Transmission
Stand alone vs. interconnected
Door Heat Exchanger: Specification
Introduction to ATA chapters ATA CHAPTERS Aircraft general - ATA Airframe systems - ATA Structure - ATA Propeller/rotor - ATA.
Presentation transcript:

Tethered Aerostats & Launch Recovery Systems Skydoc™ Systems, Inc. Tethered Aerostats & Launch Recovery Systems www.skydocballoon.com

Aerostats—helium-filled, payload-carrying balloons—can provide an aerial 24/7 surveillance and communications with increasing reliability, safety, size and carrying capacity. Size (and quality) matters: larger and higher quality aerostats can withstand rougher conditions, are safer and more durable, and carry larger, more advanced payloads, ranging from communications sensors, to EO/IR cameras.

Component sub-systems: A majority of aerostat systems will include several sub-systems (Figure): The balloon itself (the aerostat) Various “aerial unit” – the operational payload plus the hardware, communications and power systems needed to run it Operational payload – the sensors or devices performing the mission (survey, detect, communicate, etc.) Ground anchor unit that keeps the aerostat in place Operational station – where the ground controllers operate the system and payload Helium gas and support equipment to maintain the system over time

Size/Volume: The aerostat’s size, and thus its relative gas volume capacity, determines its capacity to lift the platform, cables, supporting gear and payload to its operational altitude. Size matters – larger systems generally carry heavier (read: better, longer-range) payloads and remain airborne in higher altitudes, over longer periods of time and in more challenging weather conditions than smaller ones. As you might expect, this greater capacity usually requires heavier, more complicated support structures, greater manpower and more power and helium. Payload “carrying capacity”: The weight that the aerostat can lift beyond its own and its tether’s is its payload carrying capacity. It refers to both the “operational” payload, such as a camera, and the supporting systems that must be airborne with it (e.g. power, communication, computing, lights, etc.) Operational altitude: The operational altitude is the “above ground” altitude at which the system is expected to operate while carrying the designated payload weight. Lift, and thus operational altitude, may change with external conditions, such as air pressure, and operators can lift the system to various altitudes within system limitations.

Choosing a system When considering aerostats for surveillance or communications applications, teams should investigate a range of systems (various designs, sizes, mobile and stationary) with respect to their mission, particularly in the expected area of operation. Aerostats range from small systems flown at altitudes less than 304m (1,000ft), carrying payloads under 20kg for a short range, to heavy, long-range systems elevated up to 608m (2,000’), carrying large payloads over 20kg with longer range surveillance or communications.

Operational Payloads: Aerostats are open platforms that, depending on the model and design, can carry a great variety of mission payloads. Most deployed aerostats carry electro-optical (day and night cameras) or communication (e.g. relay) payloads. Aerostat platform characteristics such as size, power and communication determine the expected payload carrying capacity and flight altitude. Larger aerostat systems with a continuous power source can carry larger, heavier payloads over longer periods of time. The operational “range” depends on the characteristics of both the aerostat platform (flight altitude) and the payload itself. The range depicted in many promotional materials relies on a specific manufacturer’s combination of components, under standardized conditions. The same aerostat platform may be able to carry different payloads, depending on needs, design of the platform, station, and payload, and conditions.

Limitations, Quality and Safety: Aerostat systems are designed to be used in the field over long periods of time. Quality of design and manufacturing are critical to ensure satisfactory field performance over time. Systems of any size that are designed to meet military standards are usually highly reliable and superior quality but carry a much greater cost. Wind, air pressure, and rain are the main external factors affecting and limiting aerostat system operation. Generally speaking, quality is indicated by the system’s ability to remain airborne over longer periods of time, in harsher weather conditions while transmitting quality payload data in the required view range. Larger, higher-quality systems require additional training and safety protocols to ensure the safe and efficient operation of both the aerostat (platform) and the mission (payload). Any system running day and night requires operators (for aerostat and payload) in shifts that will be vigilant enough to detect and respond to any disturbance. The helium used for a given aerostat must match the required quality and be available in sufficient and regular supply for continuous routine operation. Helium supply must be included in calculating the long-term cost of maintaining an aerostat system. Helium fueling/refueling requires an anchoring of the system (it cannot be done while airborne).

Blimp stability in windy conditions Winds: Very large 'blimp' aerostats can sometimes remain stable in high winds due to their massive helium lift at the bow that combats the wind. However, these very large blimps are hugely expensive and uneconomical for almost any activity. For small, less expensive blimps, the helium lift at the bow is far smaller, thus reducing blimps wind-keeping capability. This is a major reason why small blimps cannot cope with high winds. Thus large blimps that have some wind-keeping ability are too expensive, and small blimps that are more economical to use cannot cope with high winds.

Specification Information on SkyDoc™ Aerostat Products Launcher: Versatility Ground Based Platform Specialized Trailer with power for use in remote locations Width and height designed for Flatbed and Pickup Truck mobility Designed for transport in CH46, CH53 or fixed wing aircraft Equipped with lifting rings for transport by helicopter Used as on-site control center or relay to remote command station Equipment Continuous power to payload with powered aerostat tether Adaptable for HMMWV, 120/220VAC, 12V or generator electrical input Onboard air conditioning for electrical/electronic components cooling Components Aerostat cradle for secure storage or safe movement between locations Winch to launch and retrieve aerostat All electrical/electronic components to operate payload Temperature controlled equipment compartment On board battery bank and generator (2kw or 5kw) with fuel storage Lighting source (white and red) as needed for on site operations Storage compartments for helium bottles, cradle, aerostat, portable lighting and extra equipment

Specification Information on SkyDoc™ Aerostat Products Single ply material used for all but extreme weather conditions Material is polyurethane and can be 3mil, 6mil or 9mil thickness Helium loss can be up to one per cent per day depending on temperature swings and aerostat pressure The aerostat design allows for additional lift with increased wind speed and has been flown in 110 mph without incident Welders grade helium is preferred Variety of colors available Multi-ply material used for extreme weather conditions The multiple ply SkyDoc™ Aerostat has all the attributes of the single ply Helium loss is comparable to the single ply aerostat Material design is a multi-layered material with inner and outer coating for use in extreme cold weather conditions Pressure relief valve will open with increased pressure caused by increased temperature Tether: Varies in breaking strength characteristics from 250lbs (112kg) to 5000lbs (2250kg) Embedded copper wire #18 gauge up to #24 gauge is available Single optical fibers available Material is Spectra strength braid with polyester outer coating Total weight of tether is dependent on breaking strength requirements, altitude desired, if embedded copper wire/optical fiber needed

Specification Information on SkyDoc™ Aerostat Products Winch: Description: Large frame – 4 ½ “ (11.43cm) drum, 17” (43.18cm) drum ends Directional switch Various AC or DC motors available Electrical and/or fiber optic slip ring available for tether power to payload Motor brake available 3.25 Worm Center Gear Box available with 60:1 @ 1725 RPM, 35’ (10.6m), 1000lbs (450kg) pull 30:1 @ 3450 RPM, 70’ (21.3m), 650lbs (292.5kg) pull Vertical Winch: Outside Dimensions: 32.18” Width – 31.09” Height – 22.18” Depth – 350lbs net weight Winch dimensions: 8.5” Drum diameter – 9” Drum width – 18” Drum flanges Drum tether capacity: 1529’ of 0.28” tether with .5” Freeboard Electrical slip ring and Ethernet connection 15' (4.5m) Winch control pendant Control panel to include: DC meter, main DC ON/OFF switch Shore power breaker to connect external 120VAC to the DLS-30/IQ4 battery charger Main DC ON/OFF switch turns the winch on and off Battery charger DLS-30/IQ4 will connect directly to the battery 30-amp battery charger 2 SLA-1175 Marine deep cycle 75AH to provide DC power 1 each standard 120VAC 15amp shore power input receptacle Quick disconnect panels for ease of maintenance Manual (quick throw) emergency stop handle

Aerostat Launch/Recovery Options