Relevant bibliographies by topics / Flight characteristics

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Flight characteristics'

Author: Grafiati
Published: 4 June 2021
Last updated: 26 July 2025

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Journal articles on the topic "Flight characteristics"

1

PRISACARIU, Vasile. "ANALYSIS OF UAVs FLIGHT CHARACTERISTICS." Review of the Air Force Academy 16, no. 3 (2018): 29–36. http://dx.doi.org/10.19062/1842-9238.2018.16.3.4.

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Chen, Jiu Sheng, and Xiao Yu Zhang. "Modeling of Flight Arrival Scheduling Based on Fuzzy Programming." Applied Mechanics and Materials 313-314 (March 2013): 995–98. http://dx.doi.org/10.4028/www.scientific.net/amm.313-314.995.

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The issue of flight arrival in civil airport is a typical problem of discrete event dynamic system. IN Time is a random variable. According to the characteristics of arrival flights, flight delay cost as objective function, the fuzzy model for scheduling arrival flights is established. In the case of growing air traffic, the model is a better opinion for scientific optimum ordering matter in air traffic control system. It can improve flight operation on time.
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BRUDERER, BRUNO, and ANDREAS BOLDT. "Flight characteristics of birds:." Ibis 143, no. 2 (2001): 178–204. http://dx.doi.org/10.1111/j.1474-919x.2001.tb04475.x.

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Öznalbant, Zafer, and Mehmet Ş. Kavsaoğlu. "Flight control and flight experiments of a tilt-propeller VTOL UAV." Transactions of the Institute of Measurement and Control 40, no. 8 (2018): 2454–65. http://dx.doi.org/10.1177/0142331218754618.

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The purpose of this work is to present a study on the stability and control of an unmanned, fixed wing, vertical take-off and landing aerial vehicle. This airplane is driven by a fixed-pitch tilt-propeller system with the capability of vertical take-off and landing as well as conventional flight. The novelty of the vehicle is the use of a fixed-pitch propeller system instead of variable-pitch tilt-rotors. There are three flight modes: vertical, transitional and conventional flight modes. Each flight mode has different dynamic characteristics. Therefore, these modes each need dedicated flight c
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Yang, Zi-Yi, and Rong-Jiun Sheu. "EFFECTS OF FLIGHT ROUTE VARIATION AND GREAT-CIRCLE APPROXIMATION ON AVIATION DOSE ASSESSMENT FOR POPULAR FLIGHTS FROM TAIWAN." Radiation Protection Dosimetry 184, no. 1 (2018): 79–89. http://dx.doi.org/10.1093/rpd/ncy186.

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Abstract Galactic cosmic-ray-induced secondary particles in the atmosphere constitute an important source of radiation exposure to airline crews and passengers. In this study, a systematic dose assessment was conducted for 11 popular flights from Taiwan, with an emphasis on the effects of flight route variation and assumption. The case studies covered a broad range of commercial flights departing from Taipei, from a domestic flight of <1 h to a long-haul international flight of more than 14 h. For each route under study, information on 100 actual flight routes was retrieved from flight trac
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Kulba, P., V. Fedenko, O. Cherednikov, V. Chupryna, and O. Pankul. "TAKING INTO ACCOUNT THE REQUIREMENTS OF EUROPEAN CRITERIA FOR CERTIFICATION OF AIRWORTHINESS OF AIRCRAFT IN TECHNIQUES FOR TESTING THE FLIGHT-TECHNICAL CHARACTERISTICS OF HELICOPTERS." Наукові праці Державного науково-дослідного інституту випробувань і сертифікації озброєння та військової техніки, no. 10 (December 30, 2021): 108–16. http://dx.doi.org/10.37701/dndivsovt.10.2021.12.

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The article considers the problem of improving the methods of testing to determine the flight characteristics of helicopters, taking into account the requirements of European criteria for certification of airworthiness of military aircraft. To ensure interoperability with NATO standards, new standard methods for obtaining and evaluating the flight performance of helicopters have been developed. On the example of determining fuel consumption in assessing the range and duration of the flight considered the basic principles of development of advanced standard techniques.
 The test methods ar
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Burmistrov, V. I., E. I. Matkevich, and I. V. Ivanov. "Analysis of the Radiation Situation in Aviation Flights under Conditions of Solar Proton Events." MEDICAL RADIOLOGY AND RADIATION SAFETY 70, no. 3 (2025): 54–69. https://doi.org/10.33266/1024-6177-2025-70-3-54-69.

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With a general analysis of the levels of ionizing radiation characteristic of outer space and causing radiation hazard factors for astronauts, the issues of assessing the radiation situation in air travel also remain relevant. The purpose of the study was to analyze the types and characteristics of ionizing radiation in airspace up to heights of 20 km above the Ground and possible radiation doses to flight personnel during flights under these conditions. The composition of ionizing radiation and the energy characteristics of proton events are analyzed. The radiation dose rates are estimated de
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SUZUKI, Shota, Shinichiro ITO, and Masaki HIRATUKA. "Flight characteristics of flying discs." Proceedings of the Symposium on sports and human dynamics 2020 (2020): B—5–2. http://dx.doi.org/10.1299/jsmeshd.2020.b-5-2.

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Wilhelm, Frank H., and Walton T. Roth. "Clinical Characteristics of Flight Phobia." Journal of Anxiety Disorders 11, no. 3 (1997): 241–61. http://dx.doi.org/10.1016/s0887-6185(97)00009-1.

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Bader, Gail Byrne, Maureen Terhorst, Patricia Heilman, and Judith A. DePalma. "Characteristics of flight nursing practice." Air Medical Journal 14, no. 4 (1995): 214–18. http://dx.doi.org/10.1016/1067-991x(95)90005-5.

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Dissertations / Theses on the topic "Flight characteristics"

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Larsson, Roger. "System Identification of Flight Mechanical Characteristics." Licentiate thesis, Linköpings universitet, Reglerteknik, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-92823.

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With the demand for more advanced fighter aircraft, relying on relaxed stability or even unstable flight mechanical characteristics to gain flight performance, more focus has been put on model-based system engineering to help with the design work. The flight control system design is one important part that relies on this modeling. Therefore it has become more important to develop flight mechanical models that are highly accurate in the whole flight envelop. For today’s newly developed fighters, the basic aircraft characteristics change between linear and nonlinear as well as stable and unstabl
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Sopizhenko, L. A. "THE FLIGHT CHARACTERISTICS OF UNNAMED AIR VEHICLES." Thesis, Національний авіаційний університет, 2015. http://er.nau.edu.ua/handle/NAU/17211.

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This technical note presents an over view of the flight characteristics of Unmanned Air Vehicles (UAV’s). The research focuses on the various types of UAV before moving on to the associated technical requirements and innovations. The categories discussed cover flight control, navigation, propulsion, payload capability, launch and recovery, communications and airspace management. To conclude, current and future UAV development issues are also explored in light of the political and economic market.
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Kornienko, Andrei. "System identification approach for determining flight dynamical characteristics of an airship from flight data." [S.l. : s.n.], 2006. http://nbn-resolving.de/urn:nbn:de:bsz:93-opus-28803.

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Soinne, Erkki. "Aerodynamic and Flight Dynamic Simulations of Aileron Characteristics." Doctoral thesis, KTH, Aeronautical Engineering, 2000. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-3038.

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Hazlehurst, Grant Allen. "The morphometric and flight characteristics of the pterosaurs." Thesis, University of Bristol, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.303761.

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Yin, Feijia, Volker Grewe, Christine Frömming, and Hiroshi Yamashita. "Impact on flight trajectory characteristics when avoiding the formation of persistent contrails for transatlantic flights." Elsevier, 2018. https://publish.fid-move.qucosa.de/id/qucosa%3A72194.

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This paper studies the impacts on flight trajectories, such as lateral and vertical changes, when avoiding the formation of persistent contrails for transatlantic flights. A sophisticated Earth-System Model (EMAC) coupled with a flight routing submodel (AirTraf) and a contrail submodel (CONTRAIL) is used to optimize flight trajectories concerning the flight time and the flight distance through contrail forming regions (contrail distance). All the trajectories are calculated taking into account the effects of the actual and local meteorological parameters, e.g., wind, temperature, relative humi
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Neiusma, William J. Jr. "An investigation of two-propeller tilt wing V/STOL aircraft flight characteristics." Thesis, Monterey, California. Naval Postgraduate School, 1993. http://hdl.handle.net/10945/39820.

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Approved for public release, distribution is unlimited<br>The results of a two-propeller tilt wing aircraft static stability and performance simulation utilizing a NASA-Ames computer code, Tilt Wing Application General (TWANG), are presented with comparisons to actual test flight data. The Canadair CL-84 tilt wing aircraft was used as a model for the geometric data utilized by the computer simulation. Aerodynamic data for the simulation were obtained from previous NASA Ames research related to a four-propeller model. Variables used included a wide range of parameters associated with flig
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Neiusma, William J. "An investigation of two-propeller tilt wing V/STOL aircraft flight characteristics." Monterey, California : Naval Postgraduate School, 1993. http://handle.dtic.mil/100.2/ADA257751.

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Thesis (Aeronautical and Astronautical Engineer)--Naval Postgraduate School, June 1993.<br>Thesis Advisor: Newberry, Conrad F. "June, 1993." Description based on title screen as viewed on April 16, 2009. Includes bibliographical references (p. 78-79). Also available in print.
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Hrabovský, Matúš. "Posouzení letových vlastností a zatížení malého sportovního letounu po modifikaci pohonné jednotky." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2020. http://www.nusl.cz/ntk/nusl-417471.

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The thesis deals with the issue of replacement of the Rotax 912 ULS engine with the Rotax 915 iSc3 B engine and its impact on flight performance, characteristics and airframe loads of the WT 9 Dynamic. For accomplish better maneuverability tail surfaces are enlarged. Both versions of airplane with different engines and tails surfaces are quantified with respect to airframe loads and flight characteristics. The output of the diploma thesis can be used for strength design of airplane structure and stress tests of the new modification of the WT 9 Dynamic aircraft.
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Lewis, William D. "An aeroelastic model structure investigation for a manned real-time rotorcraft simulation." Diss., Georgia Institute of Technology, 1992. http://hdl.handle.net/1853/13037.

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Books on the topic "Flight characteristics"

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Rego, Ashley Titus. Simulating the response characteristics of flight instruments. Dept. of Aerospace Science and Engineering, 1985.

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Christodoulidis, Theoharis. Robustness characteristics of active flight control algorithms. University of Salford, 1987.

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Center, Ames Research, ed. Parametric study of supersonic STOVL flight characteristics. NASA Ames Research Center, 1985.

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Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Space vehicle flight mechanics. AGARD, 1990.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Space vehicle flight mechanics. AGARD, 1990.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Space vehicle flight mechanics. AGARD, 1990.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Advances in flying qualities. AGARD, 1988.

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Air Force Human Resources Laboratory., ed. Display characteristics of example light-valve projectors. Air Force Human Resources Laboratory, Air Force Systems Command, 1989.

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J, Burken John, Maine Trindel A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Flight testing a propulsion-controlled aircraft emergency flight control system on an F-15 airplane. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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Grant, Peter Robert. Motion characteristics of the UTIAS Flight Research Simulator Motion-base. Dept. of Aerospace Science and Engineering, 1985.

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Book chapters on the topic "Flight characteristics"

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Svozil, Karl. "Some Flight Characteristics." In UFOs. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-34398-8_7.

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Kopp, Gregory A. "Flight Characteristics of Wind-Borne Debris." In Wind-Borne Debris Hazards. American Society of Civil Engineers, 2018. http://dx.doi.org/10.1061/9780784414965.ch04.

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Decher, Reiner. "Putting It All Together." In The Vortex and The Jet. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_7.

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AbstractWe examine the lift and drag characteristics of wings as these are affected by the two physical aspects of flight: friction effects and for higher speed, air compressibility. We encounter the phenomenon of stall, shock waves, and visible condensation. These make flight phenomena interesting and challenging. Friction effects in supersonic flight are shown to be an almost negligibly small part of the heating of aircraft skin surfaces.
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Che, Da. "The Characteristics of Flight Test Simulator and Its Application in Civil Aircraft Flight Test." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-2440-9_39.

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Jia, Jian, Weifeng Chen, and Zixuan Wang. "Aerodynamic Parameter Estimation for Launch Vehicles." In Autonomous Trajectory Planning and Guidance Control for Launch Vehicles. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-0613-0_7.

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AbstractAerodynamic force plays an important role in the flight of space launch vehicles. Therefore, obtaining accurate aerodynamic characteristics is the basis and prerequisite for establishing an aerodynamic model and designing a vehicle with excellent characteristics.
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An, Chao, Linpu Wang, Changchuan Xie, and Chao Yang. "Aerodynamics Characteristics and Flight Dynamics Analysis of Multi-body Aircraft." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2689-1_28.

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Fang, Jian Cheng, Wen Ji Xu, Z. Y. Zhao, and L. Wang. "Influence of In-Flight Particle Characteristics on the Forming Quality." In Materials Science Forum. Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-960-1.2823.

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Song, Zhengyu, Cong Wang, and Yong He. "Autonomous Guidance Control for Ascent Flight." In Autonomous Trajectory Planning and Guidance Control for Launch Vehicles. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-0613-0_2.

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AbstractThe purpose of the guidance control is to release a payload into a prescribed target orbit (PTO) accurately. The parameters that determine an orbit are called orbital elements (OEs), which include the semi-major axis a, the eccentricity e, the argument of perigee $$\omega $$ ω , the inclination angle i, and the longitude of ascending node (LAN) or the right ascension of ascending node (RAAN) $$\Omega $$ Ω , where a and e can be converted to the perigee height $$h_p$$ h p and the apogee height $$h_a$$ h a . Thus, the guidance mission of a launcher is a typical optimal control problem wi
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Sarwade, A. G., A. S. Narayana, S. Panneerselvam, et al. "Aerodynamic characteristics of generic flight vehicle configuration from shock tunnel tests." In Shock Waves. Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/978-3-540-27009-6_18.

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Wang, Lei, Changxu Wu, and Ruishan Sun. "Pilot Operating Characteristics Analysis of Long Landing Based on Flight QAR Data." In Lecture Notes in Computer Science. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-39354-9_18.

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Conference papers on the topic "Flight characteristics"

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King, Frank, Alexander Steinwandel, and Walter Fichter. "Performance Characteristics of Symmetrized In-Flight Tracking Control." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9493.

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In this paper an in-flight tracking control system minimizing vibratory loads at the frequencies 1/rev and 2/rev using steady deflections of active trailing-edge flaps is examined. The control system is based on the relaxed HHC algorithm and uses the Moore-Penrose pseudoinverse of a symmetrized transfer matrix to calculate the control commands for vibration reduction. The focus of the current investigation is on symmetrization effects of the transfer matrices used for controller design on the performance of the control system. In a theoretical pre-flight analysis bounds for the stationary solu
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Dalmeijer, Wouter, Ivan Miletovic, Olaf Stroosma, and Marilena Pavel. "Extending the Objective Motion Cueing Test to Measure Rotorcraft Simulator Motion Characteristics." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12104.

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In search of a more objective way to evaluate motion cueing fidelity, the Objective Motion Cueing Test (OMCT) was proposed by Advani and Hosman in 2006. However, a direct application of this test for rotorcraft flight simulation has not yet been studied. The first objective of this paper is therefore to investigate the extent to which the OMCT is representative for rotorcraft simulation. The second objective is to investigate whether the OMCT can be extended to better represent helicopter motion. It was found that the current OMCT defines a set of input signals that is sufficient for predictin
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Goli, Nishanth, David Arterburn, Chris Duling, and Chris Sallis. "Modeling and Simulation of sUAS Impact Characteristics Following In-Flight Failures." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12912.

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The injury potential to a human from a descending small Unmanned Aerial System (sUAS) following an in-flight failure has a large impact on how the FAA chooses to regulate sUAS flight over people. The impact characteristics of any sUAS post in-flight failure must be known before operating over people to determine how much impact energy the vehicle may introduce during the collision. This paper focuses on Modeling and Simulation of sUAS post in-flight failure to estimate its impact characteristics. Quadrotor models of three commercial UAVs are developed. Their post failure trajectories are simul
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Zhu, Zheng, Qijun Zhao, Simeng Jing, Xin Yuan, and Bo Wang. "Analyses on Aeroacoustic Characteristics of Coaxial Rotor in Forward Flight." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12665.

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Based on CFD method and FW-Hpds equations, a numerical method for predicting aeroacoustic characteristics of coaxial rotor is established. In order to accurately simulate the flowfield of coaxial rotor, several techniques including moving-embedded grids, implicit LU-SGS scheme, ROE-MUSCL scheme and Spalart-Allmaras turbulence model are adopted to solve the RANS equations. The aeroacoustic characteristics of coaxial rotor in forward flight are calculated and analyzed by using FW-Hpds equations. The calculated acoustic characteristics of the AH-1/OLS model in forward flight for validation are in
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Yi-Yang, Ma, Zhao Qi-Jun, and Wang Bo. "Active Flow Control Strategy on Improving Aerodynamic Characteristics of Rotor." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-11998.

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A new active flow control strategy by placing a synthetic jet actuator (SJA) and a trailing-edge flap (TEF) has been proposed, and its control effects on mitigation of large negative pitching moments and drag caused by rotor dynamic stall are numerically investigated by CFD method. A moving-embedded grid method and an unsteady Reynolds averaged Navier–Stokes (URANS) solver are established for predicting the complex flowfields of rotor and airfoil. Calculated results of VR-12 and SC1095 airfoils indicate that TEF and SJ can suppress the formation of dynamic stall vortex and postpone flow separa
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Owen, Dwayne, Brian Modrzejewski, and Scott Gardner. "Improving Wear and Fretting Characteristics with Fiber Reinforced Aluminum Liners." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9630.

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A study has recently been performed to investigate improvements between the interfaces of the transmission case and rolling element bearings that provides for extended wear life. This study included demonstration testing of the improvements shown in wear and fretting characteristics at the bearing/case interface by using a Fiber Reinforced Aluminum (FRA) liner. This liner material is an engineered metal matrix composite that exhibits the best mechanical properties of each of the constituent materials, and provides enhanced capabilities in terms of structural, thermal, and chemical performance.
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TURSUN, Gokhan, Betul ERGUL, and Yusuf ULU. "Evaluation of Rotor Structural Characteristics Based On Whirl Tower Tests." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9645.

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Robust and reliable structural design necessitates numerous tests for rotor blades and rotor heads. The only way to be sure regarding analysis methods containing many assumptions and unknowns is to conduct dedicated tests simulating the operational case as close as possible. Within this context, a series of test activities have been planned so as to provide structural integrity verification of rotor system. In order to evaluate structural and aeromechanical performance of the rotor system, a Whirl Tower is designed and manufactured indigenously in TAI. In this study, an assessment on Whirl Tow
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Nguyen, Hung D., Liu Yu, and Koichi Mori. "Aerodynamic Characteristics of Quadrotor Helicopter." In AIAA Flight Testing Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-3141.

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Kay, Jacob. "Acquiring and modeling unsteady aerodynamic characteristics." In Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-3907.

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Murphy, Kelly, Robert Nowak, Richard Thompson, Brian Hollis, and Ramadas Prabhu. "X-33 hypersonic aerodynamic characteristics." In 24th Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4162.

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Reports on the topic "Flight characteristics"

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Silton, Sidra I., and Bradley E. Howell. Aerodynamic and Flight Dynamic Characteristics of 5.56-mm Ammunition: M855. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada530895.

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Deussing, Eric C., Jr Artino, Folga Anthony R., and Richard V. In-Flight Hypoxia Events in Tactical Jet Aviation: Characteristics Compared to Normobaric Training. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada530631.

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Geri, George A. Eye and Head Movement Characteristics in Free Visual Search of Flight-Simulator Imagery. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada524435.

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Das, Debopam. Aerodynamics Characteristics of Butterfly Flight Through Measurement of Three-Dimensional Unsteady Velocity Field Using TR-PIV System. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada511002.

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Lee, R. S., J. Colvin, A. Frank, L. Fried, and J. Reaugh. Final report: flight dynamics and impact characteristics of thin flyer plates driven by laser-and electrically-produced plasmas. Office of Scientific and Technical Information (OSTI), 2001. http://dx.doi.org/10.2172/15006442.

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Maslo, Brooke, Morgan Mark, Kathleen Kerwin, et al. Habitat use and foraging ecology of bats in Morristown National Historical Park: Effects of invasive vegetation. National Park Service, 2024. http://dx.doi.org/10.36967/2303689.

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Temperate insectivorous bats value high prey abundance and appropriate vegetative structure when selecting foraging habitats. Forests, particularly in the eastern United States, provide prime foraging habitats for bats but can be heavily impacted by non-native plants, which may alter arthropod diversity and abundance, as well as vegetative structure. To investigate associations between non-native plants and insect abundance, vegetative structure, and consequently bat activity, we performed vegetation surveys, insect trapping, and acoustic monitoring at 23 forested plots in northern New Jersey,
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Anderton, Gary, Ernest Berney, John Newman, Travis Mann, Chad Gartrell, and Daniel Miller. Joint Rapid Airfield Construction (JRAC) Program 2004 Demonstration Project--Fort Bragg, North Carolina. Engineer Research and Development Center (U.S.), 2021. http://dx.doi.org/10.21079/11681/40139.

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This report describes the demonstration of technologies and procedures developed during April 2002 and May 2004 under the Joint Rapid Airfield Construction (JRAC) Program. The demonstration took place at Sicily Landing Zone (LZ) at Fort Bragg, NC, in July of 2004. The objective of the exercise was to demonstrate the procedures and technologies developed under the JRAC Program by rapidly building two parking aprons capable of supporting C-130 transport aircraft taxiing and parking operations. The exercise was conducted under continuous 24-hr operations to simulate a real-world rapid constructio
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