Browse Topic: Fire suppression

Items (63)
The design, testing, and analysis of a Guided Autorotative Delivery System (GADS) for suppression of incipient wildfires is described. The GADS consists of an unpowered 1 m diameter rotor, a control unit, and a payload of 2.2 kg of fire suppressant powder. On release from a fixed-wing UAV, the rotor passively deploys and enters autorotation, decelerating the payload and allowing precise delivery of the suppressant using cyclic pitch control. A numerical model of the system was developed to calculate the trajectory of the GADS during rotor deployment and descent, in the presence of ambient wind and cyclic pitch inputs. A reduced-scale model of the rotor was tested in a wind tunnel, and an uncontrolled full-scale, 1.5 kg prototype of the GADS was fabricated and tested by dropping from a hovering quadcopter as well as a fixed-wing UAV. The full-scale drop experiments validated the deployment and autorotation stability of the system, and demonstrated that the GADS maintains descent velocities suitable for incipient fire suppression (≈ 5 m/s). Numerical predictions indicate that the GADS descent trajectory can be controlled with cyclic pitch in an ambient crosswind of at least 5 m/s (10 kts). Measurements captured during the drop tests using onboard instrumentation show good qualitative agreement with numerical predictions. Future work will include drop tests with remotely controlled cyclic pitch, followed by fully autonomous controlled descent. The study establishes design guidelines for guided autorotative systems and illustrates their potential for scalable UAV-based wildfire suppression or emergency response.
Chadha, JiaJain, RheaSakamuri, SivaThomas, ThomasSirohi, Jayant
The transition toward zero-carbon propulsion technologies has highlighted the urgent need for specialized test infrastructure to support hydrogen and alternative fuel research. This paper presents the conceptualization, design, and operation of a High-Pressure Direct Injection (HPDI) Hydrogen Internal Combustion Engine (H2 ICE) test facility with integrated ammonia fuel testing capability, marking a significant advancement in India’s sustainable automotive research efforts. Drawing from practical experience, it outlines crucial technical specifications, safety protocols, and best practices for establishing robust, adaptable, and secure testing environments. Addressing the industry’s need for dedicated infrastructure, it is engineered for adaptability across various engine types including heavy-duty, light-duty, and multi-utility vehicles while aligning with global technical standards. Key technical considerations include a transient dynamometer with an advanced automation system for precise control of both hydrogen and ammonia test cycles. Emission measurement systems such as hydrogen analyzer, ammonia-specific FTIR, particle number counter, and particle size distribution analyzer, are essential for analyzing regulated and unregulated emissions that are critical to sustainable fuel development. The hydrogen fuel storage and distribution system support up to 500 bar pressure, incorporating certified components. Three distinct supply lines operating at 350 bar (for HPDI), 100 bar (for Low Pressure Direct Injection), and 20 bar (for Port Fuel Injection) to accommodate diverse engine configurations. A separate ammonia delivery system ensures dual-fuel testing while addressing its specific chemical and safety needs. Safety remains a cornerstone of the facility's design due to hydrogen’s flammability and ammonia’s toxicity. Essential measures include a high-capacity ventilation, ATEX-rated electricals, real-time gas detection, inert-gas fire suppression, remote monitoring using CCTV, thermal imaging and acoustic sensors. The facility serves as a benchmark for hydrogen and ammonia ICE research in emerging markets, providing practical insights, and technical recommendations and guidance for aligned infrastructure development in support of a zero-carbon mobility future.
Dhyani, VipinKurien, CaneonSubramanian, BalajiKhandai, ChinmayanandaMuralidharan, M
The emergence of electric Vertical Takeoff and Landing (eVTOL) air vehicles is transforming how people and freight are moved in short distances. This transformation has a profound impact on surrounding infrastructure necessary to provide Aircraft On Ground support for eVTOLs. The hover capabilities of eVTOLs have similar operating characteristics within terminal and uncontrolled airspace. However, the need to conserve battery energy via rapid approaches and departures affects terminal airspace management. To attract eVTOL operators, existing airports, landing zones, and vertiports are modifying their infrastructure to include fixed electric charging stations, additional taxiways, upgraded fire suppression systems, separate hangers, and capable MRO facilities. Augusta Regional Airport (KAGS) is the base airport for the annual Masters Golf Tournament which experiences five times the normal airport traffic and some 40,000 commuting patrons. eVTOLs can offset land traffic issues associated with commuters and supplies. Since KAGS is centroid to 32,000 square miles of territory void of major highways, basing eVTOLs can offer expedited transit services for people and goods which will have a profound impact on the economic viability and quality of life in the area.
Stanzione, KaydonJohnston, Diane
Smoldering peat fires are the largest fires on Earth. They ignite very easily, are notoriously difficult to put out, and release up to 100 times more carbon into the atmosphere than flaming fires, contributing to climate change. These fires are known as “zombie fires” for their ability to hide and smolder underground and then reanimate as new flames days or weeks after the wildfire had been extinguished.
This SAE Aerospace Recommended Practice (ARP) provides guidelines for the effective operation and use of fire containment covers (FCCs). Technical Standard Orders (TSOs) C203 and C90e (and later revisions) incorporate AS6453, and provide the Minimum Performance Standards (MPS) for an FCC design. The net and pallet used with the FCC must be approved using the updated net and flammability requirements in TSO C90e and later revisions. However, fire containment performance also requires this equipment is properly used. Fire safety is compromised when FCCs are used in an inadequate manner.
AGE-2 Air Cargo
This SAE Aerospace Information Report (AIR) identifies and summarizes the various factors that must be considered and evaluated by the design or specifying engineer in establishing the specifications and design characteristics of battery-powered aircraft tow tractors. This AIR is presented in two parts. The first part is simply a summarization of design factors that must be considered in establishing vehicle specifications and design characteristics. The second part refers particularly to the performance characteristics of an aircraft tow tractor. Some definitions, formulas, data, and an example are provided mainly for assisting the specifying engineers of potential buyers and users of aircraft tow tractors in the evaluation and comparison of their requirements with the performance capabilities of the various tow tractors offered by the tow tractor manufacturers. Although the design engineers could also use the formulas and data in their calculations of the performance specifications of aircraft tow tractors, this AIR is not intended to provide the methods and all data necessary for detailed calculations and design of a battery-powered aircraft tow tractor.
AGE-3 Aircraft Ground Support Equipment Committee
The US Army Tank Automotive Research, Development and Engineering Center (TARDEC) has developed a unique physics based modeling & simulation (M&S) capability using Computational Fluid Dynamics (CFD) techniques to optimize automatic fire extinguishing system (AFES) designs and complement vehicle testing for both occupied and unoccupied spaces of military ground vehicles. The modeling techniques developed are based on reduced global kinetics for computational efficiency and are applicable to fire suppressants that are being used in Army vehicles namely, bromotrifluoromethane (Halon 1301), heptafluoropropane (HFC-227ea, trade name FM200), sodium-bicarbonate (SBC) powder, water + potassium acetate mixture, and pentafluoroethane (HFC-125, trade name, FE-25). These CFD simulations are performed using High Performance Computers (HPC) that enable the Army to assess AFES designs in a virtual world at far less cost than physical-fire tests. This methodology is applied to vehicle crew compartments for multiple scenarios using HFC227e + SBC powder which is the suppressant combination used in most US combat and tactical vehicles with crew fire protection systems. Predicted and test results match qualitatively very well for overall suppression time as well as for soldier survivability from thermal injury, blast overpressure and inhalation toxicity risks. After gaining confidence with crew compartment simulations, this fire suppression modeling methodology is now being applied to the geometrically-more-complex military vehicle engine compartments with HFC-125 fire suppressant that is widely used for unoccupied spaces. Challenges associated with the fire suppression simulations are discussed along with future developments that are being proposed to enhance the overall accuracy of the simulation methodology.
Korivi, VamshiMcCormick, StevenHodges, Steven
A hyperbaric chamber has been designed to achieve the goals of maximizing safety, minimizing complexity, and minimizing cost of hyperbaric chamber therapy. This design minimizes the volume of compressed gas in the chamber, and eliminates the need for complex gas mixing, carbon dioxide scrubbing, thermal management, and fire suppression systems. The simple pressurization system affords safe operation by minimally trained personnel. It requires only clean water and small volumes of compressed oxygen, and uses no electrical power. These features allow the chamber to be used in remote, undeveloped locations where hyperbaric oxygen therapy is currently not feasible.
A hyperbaric chamber has been designed to achieve the goals of maximizing safety, minimizing complexity, and minimizing cost of hyperbaric chamber therapy. This design minimizes the volume of compressed gas in the chamber, and eliminates the need for complex gas mixing, carbon dioxide scrubbing, thermal management, and fire suppression systems. The simple pressurization system affords safe operation by minimally trained personnel. It requires only clean water and small volumes of compressed oxygen, and uses no electrical power. These features allow the chamber to be used in remote, undeveloped locations where hyperbaric oxygen therapy is currently not feasible.
The use of Heavy Vehicle Event Data Recorders (HVEDRs) in collision analysis has been well recognized in past research. Numerous publications have been presented illustrating data accuracy both in normal operating conditions as well as under emergency braking conditions. These data recording devices are generally incorporated into Electronic Control Modules (ECMs) for engines or Electronic Control Units (ECUs) for other vehicular components such as the Anti-Lock Brake System. Other research has looked at after-market recorders, including publically-available Global Positioning System (GPS) devices and fleet management tools such as Qualcomm. In 2009, the National Fire Protection Association (NFPA) incorporated a Vehicle Data Recorder (VDR) component into their Standard for Automotive Fire Apparatus. The purpose of this was to “…capture data that can be used to promote safe driving and riding practices.” The Standard requires minimum data elements, recording times, and sample rates. These include vehicle speed, acceleration, throttle position, and other specified parameters. While the NFPA is not a regulatory agency, it serves to bring representatives from the fire suppression industry together to set accepted practices and standards. It was the intent of this research to validate the data imaged from a Weldon Type 6444 VDR as employed by fire vehicles. Data were compared to an external VBOX 3i measuring device, as well as internal J1939 Controller Area Network (CAN) data from the vehicle. Testing also incorporated an element designed to ensure that data were retained following a catastrophic loss of power. The results of this study demonstrate that the NFPA compliant Weldon Type 6444 as tested can be used with confidence during a collision investigation.
Austin, Timothy P.Plant, David P.LeFevre, Joseph E.
America's pony cars are a favorite of racers and fans alike, so racing them against each other is natural. Detroit's pony car category has been consistently popular with both car buyers and racing fans, so it makes sense that the U.S. automakers would pursue venues for racing their sporty 2+2s against each other. Longtime fans regard the late-1960s/early-1970s period the glory days for the Trans Am racing series because that was when Ford's Mustang, Chevrolet's Camaro, American Motors' AMX, and Dodge's Challenger engaged in legendary battles on tracks across North America.
Carney, Dan
This document applies to off-road forestry work machines defined in SAE J1116 or ISO 6814.
MTC4, Forestry and Logging Equipment
ABSTRACT Military ground vehicles are equipped with Automatic Fire Extinguishing Systems (AFES) to protect against enemy threats causing fuel tank ruptures and resulting fuel fires inside military vehicle crew compartments. The fires must be rapidly extinguished without reflash to ensure Soldier protection from burn and toxicity risks. This summary describes the development of a simulation-based acquisition tool which will complement vehicle testing for the optimization of AFES designs for specific vehicles and address their unique clutter characteristics. The simulation-based acquisition tool using Computational Fluid Dynamics (CFD) techniques was validated for an exploratory test box and demonstrated with the evaluation of two different suppressant nozzle configurations for an MRAP vehicle. The result is a cost-savings tool with a negligible development payback period that optimizes Soldier survivability in a fire situation. This modeling tool is currently being applied to predict the effectiveness of crew AFES in a number of Army ground vehicles.
Korivi, Vamshi M.Williams, Bradley A.McCormick, Steven J.Deshmukh, Kshitij
This SAE Aerospace Information Report (AIR) provides background information, technical data and related technical references for minimization of electrostatic hazards in aircraft fuel systems. Techniques used to minimize the electrostatic hazard include: a Reducing fueling rate into tank bays including use of multiple refueling inlet nozzles. b Reducing refuel plumbing flow velocities. c Introducing fuel into the tank at a low velocity near the bottom and directing it to impinge upon a grounded conducting surface. d Avoiding electrically isolated conductors in the fuel tank. e Using conductivity additives in the fuel.
AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee
This SAE Aerospace Standard (AS), identical to ISO 14186, specifies the minimum design and performance criteria and testing methods of fire containment covers (FCCs) used either: a in those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations, or b on a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not mandate their use.
AGE-2 Air Cargo
This paper presents a recently developed method meant to act as a tool for objectively assessing and comparing the performance of automatic fire suppression systems. This methodology specifies requirements and procedures for evaluating the efficiency and performance of automatic fire suppression systems permanently installed in the engine compartments of buses and coaches. The testing is done according to SP method 4912 and carried out in a test enclosure where the fire performance of different suppression systems can be objectively assessed in a well-defined way. The test methodology includes a battery of fire tests simulating different engine loads, air flows and fire scenarios. Every tested system is rated according to its performance. The test method also includes testing of re-ignition due to hot surface ignition of liquid fuels.
Brandt, JonasModin, HåkanRosen, FredrikFörsth, MichaelOchoterena, Raúl
This paper presents a fire suppression analysis for the Altair project. The architecture of the Altair systems relevant to fire safety is briefly reviewed. This is followed by an outline of a fire safety analysis of the spacecraft including an outline of a probabilistic risk analysis (PRA). The particular emphasis of this analysis is the change in risk as the vehicle moves to lower pressure, higher operating voltage and increased oxygen mole fraction. The analysis shows that all of these changes increase the likelihood and intensity of a fire. The paper then outlines the options for a suppression system followed by a trade analysis of the different options. The candidate systems include inert gas agents (nitrogen, carbon dioxide and helium), water-based systems (spray, mist and foam) and chemically active agents. Chemically active agents are included for reference purposes since they are not likely candidates for the Altair vehicles.
Dietrich, D. L.Ruff, G. A.Urban, D. L.
Jack Stands in North American Rally - A Design Proposal2008-01-297012/2/2008
ABSTRACT Rally cars are among the most technologically advanced and complex race cars, with intercooled forced induction, adaptive all wheel drive and high-feature engine management being standard features for open class racers in all major North American Rally series. This high level of technology and complexity places additional burden on the service crews and mechanics charged with the task of preparing and repairing the vehicles during the competition. As such, it is of great importance that the brief service stops (thirty minutes per FIA regulation 17.2.2 [2008]) be executed as efficiently as possible. In the pursuit of valuable seconds, rally mechanics have shown a great deal of ingenuity, creating tools and procedures which are unique to the sport. One such innovation is the peg-style jack stand. As with a typical jack stand, these devices are intended to hold the car suspended above the ground at a height allowing mobility of the mechanics under the vehicle to maneuver large components such as transmissions and differentials. It is popular practice for teams to fabricate customized jack stands, without following regulations set forth by any North American sanctioning body. The jack stands used vary from being low-quality imported purchase pieces, to highly engineered fabrications. While injuries due to jack stand failure have not been a major problem to date, it is prudent to examine the situation and explore the possibility of implementing regulations which govern these tools. The sport of Rally places great importance on the safety of the drivers and co-drivers, with exhaustive regulations regarding systems such as roll cages, helmets, safety belts and fire suppression, yet there are few regulations in place to ensure the safety of the service crews. Mechanics regularly trust their lives to the jack stands which suspend the cars above them. The following paper will explore this issue through the analysis of some exemplary, popular designs of peg-style jack stands. An alternative design, with increased strength and durability as well as reduced sensitivity to fabrication errors, ground conditions, and user errors will also be explored. This proposed design is presented with a mind towards the implementation of a regulation-mandated standardized design.
Johnston, M.Martin, K.Johrendt, J.
Fundamentals of Fire Suppression in Reduced Gravity Environments2008-01-20876/29/2008
This paper discusses the unique aspects of fire suppression in reduced (micro- and Lunar/martian) gravity environments. It builds on a trade study conducted by the Fire Prevention Detection and Suppression group at the NASA Glenn Research Center that examined the efficacy of fire suppressants in reduced gravity. The first part of the present paper reviews the differences in flame characteristics between terrestrial and extraterrestrial fires and how these characteristics change the action of a fire suppressant. Special emphasis is placed on enriched oxygen ambient environments, a condition that will routinely exist on future spacecraft and extraterrestrial habitats. The most important difference between normal gravity and reduced gravity fires is the increase in the minimum suppressant concentration (for gaseous agents in a total flooding application) required to extinguish a fire in reduced gravity compared to normal gravity. The impact of this observation is that suppressant system design guidelines based on terrestrial standards will either not be adequate or will not offer the same factor of safety in reduced gravity. The paper discussion focusses on inert gas (most suitable for total flooding applications) and water mist systems (suitable for total flooding and streaming applications), with some results for chemically active systems (e.g. Halon 1301) included for reference. Finally, the paper presents recommendations on proposed tests and standards to evaluate candidate suppressant technologies.
Dietrich, D. L.Ruff, G. A.Urban, D. L.
This document applies to off-road forestry work machines defined in SAE J1116 or ISO 6814.
MTC4, Forestry and Logging Equipment
Fire Protection on Airplanes2005-01-342910/3/2005
Airplane fire protection demands a very high level of reliability. In flight there is no escape from a fire and with an abundance of fuel and ignition sources, the threat of a fire onboard an airplane is ever present. Today's airplanes comply with existing fire protection regulations. The regulations affecting fire protection change with the advent of new technologies and experiences. This paper addresses methods for fire protection in the design of new airplanes. Prevention of a fire is the best method of fire protection, for it is best to prevent a fire than to have to deal with a fire in flight, but dealing with a fire in flight may become inevitable at one point or another. This is why fire protection methods such as passive methods and active methods are addressed. This paper addresses various fire protection methods from eliminating fuels and ignition sources to reducing flammability, from zoning and compartmentation to material selection and ventilation, from temperature control to fire detection and fire extinguishing or fire suppression systems. In addition the fire protection design basis for all areas of the airplane, from radome to the tail that include the flight deck, engines, auxiliary power unit (APU), cabin, cargo compartments, fuel tanks, lavatories, crew compartments, electrical and electronics compartment, accessory compartments and the tail compartment are discussed.
Hariram, Sham S.
Thermophysical and Fire Properties of Engine Compartment Fluids2005-01-15604/11/2005
Ignition and combustion behaviors of the engine compartment fluids are presented based on their thermophysical and fire properties. The thermophysical properties considered are flash point (Tflash), autoignition temperature (Ta), hot metal surface ignition temperature (Thot), initial boiling point (Tib) and the final boiling point (Tfb). The fire properties considered are the heat release parameter, HRP (ratio of the chemical heat of combustion, ΔHch, to heat of vaporization, ΔHv) and product release parameter, PRP (ratio of the yield of the product, yj to ΔHv). In operating vehicles, the temperatures of metal surfaces in the engine compartment exceed the Tflash, Ta, Thot, Tib and Tfb values for most of the engine compartment fluids. Thus, in vehicle crashes, the fluids are capable of starting engine compartment fires as they encounter the hot surfaces, as was observed in the crash and vehicle burn tests in the GM studies. The fire properties of the engine compartment fluids (HRP and PRP) indicate that hydrocarbon-based fluids would burn with intensity comparable to or higher than gasoline and release large amounts of CO and smoke. However, the non-hydrocarbon based fluids would burn with lower intensity than gasoline and release lower amounts of CO and smoke. Fire retardation of the engine compartment fluids is generally not practical, however, providing fire suppression system in the engine compartment and fire barriers between the engine and passenger compartments would be effective in enhancing the passenger survivability. The Tflash, Ta, Thot, Tib and Tfb values of the fluids are interrelated and thus a regulatory standard could be developed for the engine compartment fluids, where limits for only Tib, Tfb and HRP could be specified for the acceptance of the fluids.
Tewarson, Archibald
Potential Driver Exposure to Halons and Alternative Agents from On Board Fire Suppression Systems in Stock Cars2004-01-355111/30/2004
This paper presents a review of the regulatory, environmental, and health issues surrounding the use of halons as a fire suppressant and a summary of the recently completed Racecar Fire Suppressant Exposure Study by ICF Consulting, Inc., under contract with the U.S. Environmental Protection Agency (EPA) (U.S. EPA, 2004a). In 2003 the EPA learned that the SFI Foundation Inc., the organization responsible for developing safety regulations and testing requirements for numerous Performance Racing Industry (PRI) sanctioning bodies, was revising its Quality Assurance Specification for On Board Fire Suppression Systems (SFI Specification 17.1). The previous Specification 17.1 required either halon 1211 or halon 1301 to be used in these systems. Halons are ozone-depleting substances (ODS) widely used in fire protection applications and whose production and use are controlled under the Montreal Protocol and the Clean Air Act (CAA). Emissions of halons lead to destruction of the earth's protective stratospheric ozone layer. Because halons are the most potent ozone depletors of the controlled ODS, the production and import of virgin halons1 was banned in the U.S. beginning in 1994. Since then, EPA has worked with industry and other affected organizations to develop, evaluate, and support adoption of alternatives to halons through EPA's Significant New Alternatives Policy (SNAP) program. Alternatives to halons are now available and used in many new applications that formerly depended on halons. With the availability of approved alternatives, EPA was concerned that the draft of the new SFI specification still allowed for the use of halons 1211 and 1301 and that the potential risk to the driver from exposure during a discharge directly into the driver's compartment had not been fully considered. To address these concerns, EPA prepared a scoping analysis of possible fire suppressant agent concentrations that could be reached in a typical stock car due to the release under various scenarios. The study was not meant to determine acceptable quantities of an agent to be used, but to serve as an example of the type of analysis EPA believes should be considered to minimize driver exposure to potentially high concentrations of the agent. The stock car scenario was modeled after what EPA understood to be reasonable race car metrics for the National Association for Stock Car Auto Racing (NASCAR) circuits and the agents included halons 1211 and 1301 as well as SNAP approved alternatives. This application was chosen because of the similarity in the dimensions of the driver's compartments of the stock car and truck body models to those of many other sanctioning bodies. From our model, the results of the study indicated that an “as designed” release of 5 lbs. of halon 1211 or 1301 into the driver's compartment could potentially create concentrations that would kill the driver. For the alternatives, at least one agent could reach the necessary concentration for fire extinguishment within the driver compartment while not posing a risk to the driver in both the car and truck body types. In the event of a catastrophic release of all agent from the system into the driver compartment, every agent reviewed would produce a potentially lethal concentration for the driver under the conditions modeled. The finished analysis was reviewed by experts at the National Institute of Standards and Technology (NIST), Delphi Corporation, DuPont, 3M, and American Pacific, and their comments and the authors' responses are summarized in Appendix A. The results of this research have been presented to SFI as well as sanctioning bodies that use SFI's safety specifications. The goal is to promote the safe application of fire suppression agents, and the use of effective alternatives to halons 1211 and 1301.
Scharfenberg, JeremyKenny, Colm
CFD Modelling on Fire Detection and Suppression in a Columbus Rack9416076/1/1994
The Columbus fire suppression procedure is based on a centralized CO2 distribution system which injects the CO2 stored in a tank into the volume where the fire has to be extinguished. The fire is detected in each volume by means of the so-called REP (Rack Essential Package), which contains a fan and the smoke sensor. In order to assess the Fire Detection and Suppression design concept and to identify possible critical areas, Alenia Spazio - with the support of Flowsolve UK, and on behalf of EUROCOLUMBUS - has performed an analysis using a Computational Fluido-Dynamic (CFD) tool. The rack containing the water pump assembly and other electronic equipment has been chosen for the study. As far as the Fire Detection is concerned, the simulation intends to predict the flow field established in the rack by the ventilation system and the transport of smoke by this velocity field from a supposed point source. The smoke from any fire within the rack must be transported to the sensor so the fire can be detected within a “reasonable” time. The Fire Suppression System has more stringent targets to meet: the CO2 must reach a 50% concentration by volume everywhere in the rack within 60 seconds. The aim of the CFD simulation was to study various combinations of CO2 nozzle and pressure relief vent positions and numbers so that the configurations which fulfill the 50% requirement can be determined. The simulation has been performed using the 1.6.5 version of the PHOENICS general-purpose CFD code.
Veneri, RuggeroParodi, PaolaGlynn, DavidTaylor, Kate
Columbus APM Environmental Control System Overview: Space Station and APM Restructuring Consequences9413056/1/1994
This paper describes the main changes affecting the APM Environmental Control System (ECS) as a consequence of the Space Station Freedom (SSF) restructuring and Columbus APM overall reconfiguration. The main purposes of this reconfiguration are: minimize the number and complexity of the interfaces with Space Station Freedom (SSF) centralize avionics command and monitoring tasks revisit the failure tolerance concept of some ECS functions unify/standardize similar functions in the two subsystem adjust lifetime requirements and simplify maintenance concept of equipment. The APM ECS consists of the following functions: active thermal control (ATCS) passive thermal control (PTCS) atmosphere pressure and composition control air revitalization and cabin ventilation temperature and humidity control vacuum and venting nitrogen supply fire detection and suppression. The new ATCS configuration provides a cooling capability for a reduced number of P/L racks by means of its moderate loop. No modification is envisaged on the low temperature loop. Failure cases on both SSF thermal buses and APM ATCS have been considered and assessed, resulting in an optimization of the ATCS operation in off-nominal modes. Due to the adoption of a new APM launcher (ARIANE 5) instead of NSTS, the Negative Pressure Relief function is no longer required. A new cabin loop architecture is considered based on the use of three fans for air distribution in the APM thermal conditioning and air exchange with the adjacent SSF node (Intermodule Ventilation). As far as the Vacuum and Venting system is concerned, the only changes are the reduction of the connected lateral P/L racks and the deletion of the venting interface with the SSF. The same lateral P/L racks are also connected to the Nitrogen Supply system with the deletion of the relevant interface valves. The main change in the Fire Detection system concerns the new location of smoke detectors within the cabin loop. The Fire Suppression system is impacted due to the reduction of the number of enclosures requiring a fire suppression capability. Optimization in heater control has been achieved, while the decentralized valve control concept has been deleted in favour of a centralized one via Power Distribution Unit (PDU).
Gargioli, EugenioBalocco, PaoloNava, LucaLeiseifer, Hans PeterSarri, Giuseppe
Conceptual Considerations on Crew Aspects in Rescue Type Space Vehicles9413116/1/1994
Latest developments of the manned European space transportation system programs have shifted emphasis from the winged vehicles (HERMES) towards unwinged, capsule type vehicles like the Assured Crew Return Vehicle (ACRV) or the Crew Transfer Vehicle (CTV). While the work on the CTV is still in an early stage, a Phase A study was performed on the ACRV in late 1992 to 1993, detailing already the major subsystem layouts, among these the Environmental Control and Life Support System and Crew Systems such as crew seats, transport couches for injured crew members or displays and controls. Due to the particular set of requirements on this rescue vehicle, it quickly became evident that optimal layouts of these crew aspect subsystems are not necessarily easily transferable from rather well known designs of e.g. a space station. Instead, different and specific requirements such as: flexibility in accommodation of a crew from 1 to 8 members in a small confinement limited volume and power provision of a shirt sleeve environment inside the vehicle medical facilities for the treatment of ill or injured crew members long dormant mode of the vehicle attached to the space station rapid activation of the vehicle in case of an emergency also require specific solutions, which may significantly differ from the known standards. Some examples of those features favoured for a rescue vehicle are: simple, reliable solutions for atmosphere temperature and humidity control including for instance a passive humidity removal by consumables specific features for contaminant removal, in particular for the event of a fire suppression.
Knorr, WolframStrittmatter, RolfTamburini, Primo
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