The median altitude exposure for all flights was 6,214 feet (1894 m). Cabin altitudes ranged from sea level to 8,915 feet (2717 m). Inspired partial pressure of oxygen falls from 159 mm Hg at sea level to 127 mm Hg at 6,200 feet and further declines to 113 mm Hg at 9,000 ft.But as power drops off, aircraft fly slower, and with stall speeds increasing with altitude, the spread between stall and maximum mach can be very small. That was the case with early Learjets. The closer to stall, the higher your wing angle to your flight path, and that increases drag, so sometimes a lower altitude is more fuel efficient.Feb 18, 2017 · Commercial airport runways are typically 2 to 4 feet thick with layers of asphalt. Taxiways are usually thinner, with around 18 inches of concrete. [2] Airplanes typically fly at an altitude of around 35,000 feet. If Earth were the size of a desktop globe, a plane at that height would be flying at only 1/10 of an inch off the surface. [2] (1) It is supplied with airspeed, altitude, and directional data obtained from sources that meet the accuracy requirements of Secs. 29.1323, 29.1325, and 29.1327, as applicable; (2) The vertical acceleration sensor is rigidly attached, and located longitudinally within the approved center of gravity limits of the rotorcraft;Commercial aircraft typically fly between 31,000 and 38,000 feet — about 5.9 to 7.2 miles — high and usually reach their cruising altitudes in the first 10 minutes of a flight, according to Beckman. Planes can fly much higher than this altitude, but that can present safety issues.You are flying an F-117A fully equipped, which means that your aircraft weighs 52,500 pounds. You want to maintain equilibrium in straight and level flight at an altitude of 30,000 feet, cruising at 400 knots to conserve fuel. The aircraft's wing area is 1,140 square feet.According to these definitions the transition layer is 0-500 feet (0-152 m) thick. Aircraft are not normally assigned to fly at the "'transition level'" as this would provide inadequate separation from traffic flying on QNH at the transition altitude. Instead, the lowest usable "'flight level'" is the transition level plus 500 ft.an airplane is flying an altitude of 10,000 feet. the pilot wants to make a smooth decent to the runway at a constant angle of 4 degrees. how far from the runway should the pilot begin the decent?-----His distance on the ground from the touchdown point is 10000*cot(4) =~ 143007 feet =~ 23.52 nautical miles (planes use knots and nautical miles) ...Let h be the length of the hypotenuse. sin C = Opposite hypotenuse sin 10 0 = 30,000 h = 30,000 sine 10 h = 30,000 0.173648 h = 172,763 feet The missing measure is the length of the hypotenuse and given measure of is 10 0 , then the measure of is 80 0 .An airplane is flying at an altitude of 12 km at 100 m/s. What is the equivalent velocity of the aircraft? Multiple choices: A. 991 m/s B. 50 m/s C. 105 m/s D. 45 m/s E. 46 m/s F. 25 m/s G. 110 m/s.= molar mass of Earth's air = 0.0289644 [kg/mol] Earth's Atmosphere Due to the fact that Earth's atmosphere experiences different rates of heating and cooling through each of its layers, these equations help to model this through the use of the temperature lapse rate, which is the rate at which temperature changes through altitude change.Answer (1 of 5): From the pilot's perspective, it's six miles from the airport. Pilots generally only care about slant range (as opposed to ground track distance) when measuring distance to a VOR/DME station, in which case the rule of thumb is that for every 1000′ of altitude, if the airplane is ...Most airplanes fly above Mean Sea Level altitudes (MSL), the altimeter would read 5,280 feet in Denver. They are corrected for barometric pressure. When flying above 18,000 feet in the U.S., airplanes express altitude in terms of Flight Levels, which have a standard altimeter setting of 29.92 inches of Mercury.(1) It is supplied with airspeed, altitude, and directional data obtained from sources that meet the accuracy requirements of Secs. 29.1323, 29.1325, and 29.1327, as applicable; (2) The vertical acceleration sensor is rigidly attached, and located longitudinally within the approved center of gravity limits of the rotorcraft;...the right scoop

Correct answers: 2 question: A passenger in an airplane flying at an altitude of 37,000 feet sees two towns directly to the west of the airplane. The angles of depression to the towns are 32 degrees nd 76 degrees How far apart are the towns? Round to the nearest mile. (1 mile = 5280 feet)But as power drops off, aircraft fly slower, and with stall speeds increasing with altitude, the spread between stall and maximum mach can be very small. That was the case with early Learjets. The closer to stall, the higher your wing angle to your flight path, and that increases drag, so sometimes a lower altitude is more fuel efficient.An airplane flying at an altitude of $10,000$ feet passes directly over a fixed object on the ground. One minute later, the angle of depression of the object is $42^{\circ} .$ Approximate the speed of the airplane to the nearest mile per hour.aircraft flying on an IFR flight plan be separated by at least one thousand feet. This formula, as basic as it seems, provides a safer air space. Any aircraft flying a heading of East - including North, Northeast, East or Southeast (0 degrees through 179 degrees) - must be at an odd altitude (3000', 5000', 13000', etc.).= molar mass of Earth's air = 0.0289644 [kg/mol] Earth's Atmosphere Due to the fact that Earth's atmosphere experiences different rates of heating and cooling through each of its layers, these equations help to model this through the use of the temperature lapse rate, which is the rate at which temperature changes through altitude change.aircraft flying on an IFR flight plan be separated by at least one thousand feet. This formula, as basic as it seems, provides a safer air space. Any aircraft flying a heading of East - including North, Northeast, East or Southeast (0 degrees through 179 degrees) - must be at an odd altitude (3000', 5000', 13000', etc.).According to these definitions the transition layer is 0-500 feet (0-152 m) thick. Aircraft are not normally assigned to fly at the "'transition level'" as this would provide inadequate separation from traffic flying on QNH at the transition altitude. Instead, the lowest usable "'flight level'" is the transition level plus 500 ft.FAA Guide to Low-Flying Aircraft The Federal Aviation Administration (FAA) is the government agency responsible for aviation ... an altitude of 1,000 feet above the highest obstacle within a horizontal radius of 2,000 feet of the aircraft. (c) Over other than congested areas - An altitude of 500 feet above the surface except over ...Transcribed image text: 6· 0-12 points An airplane is flying level at an altitude of 3000 feet and a speed of 200 ft/sec. It is about to pass over a radar station on the ground, as shown below. The dashed line represents the llne-of-sight from an operator In the radar statlon to the alrplane. airplane 3000 ft radar station How fast is the distance between the station and the airplane changing ...Apr 08, 2022 · Manage the speed of the airplane. Every airplane has an engine power setting optimized for the cruise phase of flight. Once you've reached your desired altitude, this power should be set to around 75%. Trim the aircraft for straight and level flight. You will feel the controls become smoother as you trim the plane. A new hypersonic surveillance aircraft is capable of flying at Mach 10 at 100,000 feet (Std Day). At this rate how fast can it transit from Los Angeles to New York (2500 nm)? Hint: First, find the Speed of Sound (in ft/sec), then determine the aircrafts velocity by v = Ma. Then convert to knots (nm/ hour). Now remember velocity is distance per ...FAA Guide to Low-Flying Aircraft The Federal Aviation Administration (FAA) is the government agency responsible for aviation ... an altitude of 1,000 feet above the highest obstacle within a horizontal radius of 2,000 feet of the aircraft. (c) Over other than congested areas - An altitude of 500 feet above the surface except over ...Consider a turbojet-powered airplane flying at a standard altitude of 40,000 ft at a velocity of 530 mi/h. The turbojet engine has inlet and exit areas of 13 and 10 ft 2, respectively.The velocity and pressure of the exhaust gas at the exit are 1500 ft/s and 450 lb/ft 2, respectively.Calculate the thrust of the turbojet.= molar mass of Earth's air = 0.0289644 [kg/mol] Earth's Atmosphere Due to the fact that Earth's atmosphere experiences different rates of heating and cooling through each of its layers, these equations help to model this through the use of the temperature lapse rate, which is the rate at which temperature changes through altitude change.an airplane is flying an altitude of 10,000 feet. the pilot wants to make a smooth decent to the runway at a constant angle of 4 degrees. how far from the runway should the pilot begin the decent?-----His distance on the ground from the touchdown point is 10000*cot(4) =~ 143007 feet =~ 23.52 nautical miles (planes use knots and nautical miles) ......jobs amazon

A fighter plane flying horizontally at an altitude of 1. 5 k m with speed 7 2 0 k m / h passes directly overhead an anti-aircraft gun. At what angle from the vertical should the gun be fired for the shell with muzzle speed 6 0 0 m s − 1 to hit the plane ? At what minimum altitude should the pilot fly the plane to avoid being hit ? (T a k e g ...The median altitude exposure for all flights was 6,214 feet (1894 m). Cabin altitudes ranged from sea level to 8,915 feet (2717 m). Inspired partial pressure of oxygen falls from 159 mm Hg at sea level to 127 mm Hg at 6,200 feet and further declines to 113 mm Hg at 9,000 ft.Answer (1 of 4): on average the temperature drops about 2 degrees c per 1000 feet. The actual temperature change varies with humidity, of which relative humidity and dew point are indicators. but 32 800 feet (10 000 m) is pretty cold , 66 degrees colder by that math (-33 degrees Celsius) which s...An airplane is flying at an altitude of 10,000m.The pilot sees two ships A and B.Ship A is due south of P and 22.5km away (in a direct line).Likewise ship B is due East and 40.8km from P. The height is Physics An airplane is flying North with a velocity of 22 m/s. A strong wind is blowing East at 50 m/s.Transcribed image text: 6· 0-12 points An airplane is flying level at an altitude of 3000 feet and a speed of 200 ft/sec. It is about to pass over a radar station on the ground, as shown below. The dashed line represents the llne-of-sight from an operator In the radar statlon to the alrplane. airplane 3000 ft radar station How fast is the distance between the station and the airplane changing ...4. An airplane flying at an altitude of 10 miles passes directly over a radar antenna. When the airplane is 15 miles away, the radar detects that the distance is changing at a rate of 250 miles per hour. What is the speed of the airplane? @ c = 15/ 53 dc db db zsO IS AIS -(0 10 5.Repeat for each altitude of interest and for range of airspeeds. V = 100 ft/sec - 800 ft/sec (Values depend on aircraft) Altitude Density 0 (sea level) 0.002377 slug/ft3 2. Calculate Thrust Available at same altitude and airspeed range For low bypass turbojet, the thrust math model is given by: For 10,000 ft maximum throttle setting, 3.Solve the problem.A formula for calculating the distance, d, one can see from an airplane to the horizon on a clear day is where x is the altitude of the plane in feet and d is given in miles. How far can one see in a plane flying at 20,000 feet? Round your answer to the nearest tenth mile, if necessary.5. An airplane is flying at an altitude of 8,000 feet with a speed of 600 feet per second. If the airplane's flight path would take it directly over a selected target on the ground, from how far downrange must a payload be dropped in order for it to land on the target? Neglect air resistance.in this problem, a fighter plane is flying horizontally at an altitude of 1.5 kilometer. So let us say this is the airplane, okay? Which is flying at an altitude of 1.5 kilometer. Mhm. With the speed 7 20 kilometers per hour. There is an anti uh there is an anti aircraft missile which is a direct which is kept on the ground. And it uh Jack's missile at a speed off to muzzle speed of 600 m per ...The speed of sound is not a constant, but depends on altitude (or actually the temperature at that altitude). A plane flying Mach 1.0 at sea level is flying about 1225 km/h (661 Knots, 761 mph), a plane flying Mach 1.0 at 30000 ft is flying 1091 km/h (589 knots, 678 mph) etc. Speeds below Mach 1 are called subsonic, between Mach 0.8-1.2 ...An aircraft is flying at an altitude of 32000 feet at a speed of 500 knots. What pressure difference will be produced with a pitot-static probe at this height and speed? Use the standard atmospheric model and assume that 1 foot = 0.305m and 1 knot = 0.514 m s-1. Give your answer in kPa to 2 s.f.Roger Murdock: Flight 2-0-9'er, you are cleared for take-off. Captain Oveur: Roger! Roger Murdock: Huh? Tower voice: L.A. departure frequency, 123 point 9'er. Captain Oveur: Roger! Roger Murdock: Huh? Victor Basta: Request vector, over. Captain Oveur: What? Tower voice: Flight 2-0-9'er cleared for vector 324. Roger Murdock: We have clearance ... Answers: 2 on a question: An airplane flying at an altitude of 30,000 feet flies up to avoid a storm. Immediately after passing the storm, the airplane returns to its original altitude. What integer represents the airplane's change in altitude to avoid the storm? What integer represents the airplane's change in altitude immediately after passing the storm?Cabin altitude is defined as— Cabin pressure, in terms of altitude, above the mean sea level, while the aircraft cruising at a certain altitude. This will become more clear from the following statement— An aircraft cruising at an altitude of 37000 feet has a Cabin Altitude of 8000 feet.All aircraft flying above 18,000 feet MSL are required to set their altimeters to 29.92 inches Hg (in the US). This means that all aircraft flying in the flight levels will have the same altimeter setting. Swayne Martin 3) Density Altitude Density altitude is pressure altitude corrected for non-standard temperature....how to lose weight in a week at home

An airplane is flying at an altitude of 33,000 feet. It needs to reduce its altitude by 6% to avoid some turbulence. After it passes the turbulence, it increases its altitude by 5000 feet. What is the final altitude of the airplane? Enter your answer in the box. Advertisement Answer 5.0 /5 7 reinhard10158 Step-by-step explanation: 100% = 33,000 ftAn airplane is flying with a constant altitude at a speed of 450 mph in a direction 10° north of west directly towards its final destination. The airplane then encounters wind blowing at a steady 34 mph in a direction 85° north Math A plane was flying at an altitude of 30,000 feet when it began the descent toward the airport.When an airplane leaves the runway, its angle of climb is 160 and its speed is 300 feet per second. Find the plane's altitude relative to the runway (in feet) after one minute. Round your answer to the nearest foot.. Draw a picture. 31 A ship leaves port at noon and has a bearing of S 270 W . The ship sails at 25 knots. How many nautical milesaircraft flying on an IFR flight plan be separated by at least one thousand feet. This formula, as basic as it seems, provides a safer air space. Any aircraft flying a heading of East - including North, Northeast, East or Southeast (0 degrees through 179 degrees) - must be at an odd altitude (3000', 5000', 13000', etc.).Commercial aircraft typically fly between 31,000 and 38,000 feet — about 5.9 to 7.2 miles — high and usually reach their cruising altitudes in the first 10 minutes of a flight, according to Beckman. Planes can fly much higher than this altitude, but that can present safety issues.At 100,000 feet, which is the cruising altitude of the Altair UAV, the graph suggests a neutron flux of about 1.0 neutrons/cm2/sec, so the flux is 1.0/0.35 = 2.9 times stronger at 100,000 feet than at 30,00 feet, and the time between upsets would be about 6.7/2.9 = 2.3 hours.Chapter CH4 Problem 27P An airplane is flying at a pressure altitude of 10 km with a velocity of 596 m/s. The outside air temperature is 220 K. What is the pressure measured by a Pitot tube mounted on the nose of the airplane? Step-by-step solution 100% (8 ratings) for this solution Step 1 of 3 Speed of sound is expressed as, …… (1)An airplane is flying at an altitude of 12 km at 100 m/s. What is the equivalent velocity of the aircraft? Multiple choices: A. 991 m/s B. 50 m/s C. 105 m/s D. 45 m/s E. 46 m/s F. 25 m/s G. 110 m/s.Correct answers: 2 question: A passenger in an airplane flying at an altitude of 37,000 feet sees two towns directly to the west of the airplane. The angles of depression to the towns are 32 degrees nd 76 degrees How far apart are the towns? Round to the nearest mile. (1 mile = 5280 feet)Start descent at three times your altitude to lose in thousands of feet to achieve a three degree gradient. Top of Descent (2.5°) ... Wind Angle = 10° x 0.5 (sine 30°) WCA = 5° Heading = 355° ... For example, flying a 3,000-pound-gross airplane at 2,400 pounds, a 20-percent reduction in weight, reduce the applicable speeds by 10 percent to ...2.24 Calculate the density altitude for an aircraft at an airport with a pressure altitude of 5,000 feet when the current temperature is 13 degrees C. 6,000 feet 2.25 Using Table 2.1, calculate the dynamic pressure, q, at 8,000 feet density altitude and 250 knots TAS.4. An airplane flying at an altitude of 10 miles passes directly over a radar antenna. When the airplane is 15 miles away, the radar detects that the distance is changing at a rate of 250 miles per hour. What is the speed of the airplane? @ c = 15/ 53 dc db db zsO IS AIS -(0 10 5.an airplane flying at an altitude of 6 miles passes directly over a radar antenna. when the airplane is 10 miles away, the radar detects that the distance s is changing at a rate of 240 miles per ......top xbox games 2014

Because the speed of sound increases with air temperature, and air temperature generally decreases with altitude, the true airspeed for a given Mach number generally decreases with altitude. As an airplane moves through the air faster, the airflow over parts of the wing will reach speeds that approach Mach 1.0. 5. An airplane is flying at an altitude of 8,000 feet with a speed of 600 feet per second. If the airplane's flight path would take it directly over a selected target on the ground, from how far downrange must a payload be dropped in order for it to land on the target? Neglect air resistance.A I is our indicated altitude, in feet. A I k is our indicated altitude, in thousands of feet. A T = ( 4 × A I k × Δ I S A) + A I. A T = ( 4 × 19 × 8) + 19000. A T = 608 + 19000. A T = 19608. In some cases, a question might ask for true altitude based on a pressure altitude, instead of an indicated altitude.An airplane is flying at an altitude of 6 miles (approximately 32,000 feet) toward a point directly above where you are standing. If you are standing x miles away from a spot that is perpendicular to the plane, what is the equation that relates the angle as a function of x? ... Or, 2 x + 0 = 414 mph. ∴ x = i,e x = 207 mph. So, The speed of ...Planes flying below 18,000 feet set their altimeter to a reported pressure setting. This allows pilots to know their altitude compared to sea level. In the flight levels, the altitude is set by reference to a standard barometric pressure of 29.92 so as to create a standard reference for all aircraft and avoid any variation. The Winds Aloft(1) It is supplied with airspeed, altitude, and directional data obtained from sources that meet the accuracy requirements of Secs. 29.1323, 29.1325, and 29.1327, as applicable; (2) The vertical acceleration sensor is rigidly attached, and located longitudinally within the approved center of gravity limits of the rotorcraft;The 60,000 feet limit was surpassed around the end of the second world war with the advent of rocket and turbojet engines. Two notable achievements: The rocket powered X-15 reached space twice. In 1963 it climbed to 67 miles, nominally corresponding to FL3530. Note that the X-15 did not self-start. The glider (!)An airplane is flying at an altitude of 33,000 feet. It needs to reduce its altitude by 6% to avoid some turbulence. After it passes the turbulence, it increases its altitude by 5000 feet. What is the final altitude of the airplane? Enter your answer in the box. Advertisement Answer 5.0 /5 7 reinhard10158 Step-by-step explanation: 100% = 33,000 ftPlanes flying below 18,000 feet set their altimeter to a reported pressure setting. This allows pilots to know their altitude compared to sea level. In the flight levels, the altitude is set by reference to a standard barometric pressure of 29.92 so as to create a standard reference for all aircraft and avoid any variation. The Winds Aloft2.24 Calculate the density altitude for an aircraft at an airport with a pressure altitude of 5,000 feet when the current temperature is 13 degrees C. 6,000 feet 2.25 Using Table 2.1, calculate the dynamic pressure, q, at 8,000 feet density altitude and 250 knots TAS....cats called

Transcribed image text: 6· 0-12 points An airplane is flying level at an altitude of 3000 feet and a speed of 200 ft/sec. It is about to pass over a radar station on the ground, as shown below. The dashed line represents the llne-of-sight from an operator In the radar statlon to the alrplane. airplane 3000 ft radar station How fast is the distance between the station and the airplane changing ...An airplane, flying horizontally at 200 mph at an altitude of 3 miles, passes over a radar station. What is the rate of change of the angle of elevation betw...Which is all a roundabout way of explaining that if this plane was flying at 29,000 feet an hour after departure, it was probably just the first step in its pre-programmed series of staggered cruise altitudes, based on fuel, passenger and cargo loads, econ cruise speeds at altitude, winds, etc. as computed by the FMC.According to these definitions the transition layer is 0-500 feet (0-152 m) thick. Aircraft are not normally assigned to fly at the "'transition level'" as this would provide inadequate separation from traffic flying on QNH at the transition altitude. Instead, the lowest usable "'flight level'" is the transition level plus 500 ft.Roger Murdock: Flight 2-0-9'er, you are cleared for take-off. Captain Oveur: Roger! Roger Murdock: Huh? Tower voice: L.A. departure frequency, 123 point 9'er. Captain Oveur: Roger! Roger Murdock: Huh? Victor Basta: Request vector, over. Captain Oveur: What? Tower voice: Flight 2-0-9'er cleared for vector 324. Roger Murdock: We have clearance ... Most airplanes fly above Mean Sea Level altitudes (MSL), the altimeter would read 5,280 feet in Denver. They are corrected for barometric pressure. When flying above 18,000 feet in the U.S., airplanes express altitude in terms of Flight Levels, which have a standard altimeter setting of 29.92 inches of Mercury.To find how far to the airport, we want to find the hypotenuse of the right triangle (See image). To find this we can use the sine ratio. ≈ The ground distance can be found by using the tangent...Question 1118869: A small airplane at an altitude of 5000 feet is flying East at 300 feet per second, and you are watching it with a small telescope as it passes directly overhead. Refer to the figure above. a. What is the slope of the telescope 5, 10, and 20 seconds after the plane passes overhead? b.A fighter plane flying horizontally at an altitude of 1. 5 k m with speed 7 2 0 k m / h passes directly overhead an anti-aircraft gun. At what angle from the vertical should the gun be fired for the shell with muzzle speed 6 0 0 m s − 1 to hit the plane ? At what minimum altitude should the pilot fly the plane to avoid being hit ? (T a k e g ...(1) It is supplied with airspeed, altitude, and directional data obtained from sources that meet the accuracy requirements of Secs. 29.1323, 29.1325, and 29.1327, as applicable; (2) The vertical acceleration sensor is rigidly attached, and located longitudinally within the approved center of gravity limits of the rotorcraft;All aircraft flying above 18,000 feet MSL are required to set their altimeters to 29.92 inches Hg (in the US). This means that all aircraft flying in the flight levels will have the same altimeter setting. Swayne Martin 3) Density Altitude Density altitude is pressure altitude corrected for non-standard temperature.IFR Pilots flying on a magnetic course (track) of 0 degrees through 179 degrees should fly on an odd thousand foot MSL altitude. Example IFR Cruising altitudes would be 5,000 feet, 7,000 feet, 9,000 feet etc. IFR Pilots flying on a magnetic course (track) of 180 degrees through 359 degrees should fly on an even thousand foot MSL altitude.a passenger in an airplane flying at an altitude of h=29000 feet sees two towns directly to the left of the plane. if the respective angles of depression are theta1= 22 degrees and theta2= 58 degrees, determine the distance (in miles) between the two towns Distance between towns: Approximately feet, or , or 6.03 ≈ miles You can do the check!!10. An airplane flying 390 feet per second at an altitude of 5000 feet flew directly over an observer. The image shows the relationship of the airplane to the observer at a later time. a.) Find an equation relating x and y. 5000t 390 ce Б000 b.) Find the value of x when y is 6,250. Observer c.)= molar mass of Earth's air = 0.0289644 [kg/mol] Earth's Atmosphere Due to the fact that Earth's atmosphere experiences different rates of heating and cooling through each of its layers, these equations help to model this through the use of the temperature lapse rate, which is the rate at which temperature changes through altitude change.2.24 Calculate the density altitude for an aircraft at an airport with a pressure altitude of 5,000 feet when the current temperature is 13 degrees C. 6,000 feet 2.25 Using Table 2.1, calculate the dynamic pressure, q, at 8,000 feet density altitude and 250 knots TAS.The Mexican capital's airport has an altitude of 7,342 feet and some long-distance services can't fly there directly. This is due to the city's climate and height changing the air density, causing the need for a longer runway for larger aircraft to operate on. Therefore, routes are often broken up using smaller aircraft along the way....open fasboot on samsungna51

ratings authorized to be placed thereon. The civil aircraft fleet consists of numerous aircraft capable of high-altitude flight. Certain knowledge elements of high-altitude flight are essential for the pilots of these aircraft. As required by 14 CFR § 61.31, pilots who fly at altitudes at orCollision between a vulture and an aircraft at an altitude of 37,000 feet.-On 29 November 1973, a Riippell's Griffon (Gyps rueppellii) collided with commercial aircraft at 37,000 ft over Abijan, Ivory Coast, western Africa. The altitude is that recordedAt 100,000 feet, which is the cruising altitude of the Altair UAV, the graph suggests a neutron flux of about 1.0 neutrons/cm2/sec, so the flux is 1.0/0.35 = 2.9 times stronger at 100,000 feet than at 30,00 feet, and the time between upsets would be about 6.7/2.9 = 2.3 hours.a passenger in an airplane flying at an altitude of h=29000 feet sees two towns directly to the left of the plane. if the respective angles of depression are theta1= 22 degrees and theta2= 58 degrees, determine the distance (in miles) between the two towns Distance between towns: Approximately feet, or , or 6.03 ≈ miles You can do the check!!The speed of sound is not a constant, but depends on altitude (or actually the temperature at that altitude). A plane flying Mach 1.0 at sea level is flying about 1225 km/h (661 Knots, 761 mph), a plane flying Mach 1.0 at 30000 ft is flying 1091 km/h (589 knots, 678 mph) etc. Speeds below Mach 1 are called subsonic, between Mach 0.8-1.2 ...The 60,000 feet limit was surpassed around the end of the second world war with the advent of rocket and turbojet engines. Two notable achievements: The rocket powered X-15 reached space twice. In 1963 it climbed to 67 miles, nominally corresponding to FL3530. Note that the X-15 did not self-start. The glider (!)An airplane is flying with a constant altitude at a speed of 450 mph in a direction 10° north of west directly towards its final destination. The airplane then encounters wind blowing at a steady 34 mph in a direction 85° north Math A plane was flying at an altitude of 30,000 feet when it began the descent toward the airport.Consider a turbojet-powered airplane flying at a standard altitude of 40,000 ft at a velocity of 530 mi/h. The turbojet engine has inlet and exit areas of 13 and 10 ft 2, respectively.The velocity and pressure of the exhaust gas at the exit are 1500 ft/s and 450 lb/ft 2, respectively.Calculate the thrust of the turbojet.According to these definitions the transition layer is 0-500 feet (0-152 m) thick. Aircraft are not normally assigned to fly at the "'transition level'" as this would provide inadequate separation from traffic flying on QNH at the transition altitude. Instead, the lowest usable "'flight level'" is the transition level plus 500 ft.The speed of sound is not a constant, but depends on altitude (or actually the temperature at that altitude). A plane flying Mach 1.0 at sea level is flying about 1225 km/h (661 Knots, 761 mph), a plane flying Mach 1.0 at 30000 ft is flying 1091 km/h (589 knots, 678 mph) etc. Speeds below Mach 1 are called subsonic, between Mach 0.8-1.2 ...An airplane is flying at an altitude of 10,000m.The pilot sees two ships A and B.Ship A is due south of P and 22.5km away (in a direct line).Likewise ship B is due East and 40.8km from P. The height is Physics An airplane is flying North with a velocity of 22 m/s. A strong wind is blowing East at 50 m/s.An aircraft is flying at an altitude of 32000 feet at a speed of 500 knots. What pressure difference will be produced with a pitot-static probe at this height and speed? Use the standard atmospheric model and assume that 1 foot = 0.305m and 1 knot = 0.514 m s-1. Give your answer in kPa to 2 s.f.An airplane is flying at an altitude of 10,000m.The pilot sees two ships A and B.Ship A is due south of P and 22.5km away (in a direct line).Likewise ship B is due East and 40.8km from P. The height is Physics An airplane is flying North with a velocity of 22 m/s. A strong wind is blowing East at 50 m/s....dietary server jobs near me

Solve the problem.A formula for calculating the distance, d, one can see from an airplane to the horizon on a clear day is where x is the altitude of the plane in feet and d is given in miles. How far can one see in a plane flying at 20,000 feet? Round your answer to the nearest tenth mile, if necessary.The higher the better. One of the central reasons behind aircraft altitude is that, as the air gets thinner with every foot climbed, planes can travel more easily and therefore move faster and ...Solve the problem.A formula for calculating the distance, d, one can see from an airplane to the horizon on a clear day is where x is the altitude of the plane in feet and d is given in miles. How far can one see in a plane flying at 20,000 feet? Round your answer to the nearest tenth mile, if necessary.A private jet pilot will choose the optimum cruising altitude depending on the distance of the journey. As a rule of thumb you cross a zero off the distance in miles to calculate the optimum altitude in feet. So if you are flying 100 miles, you cross off the last zero (10) and then multiply by 1 000, giving am optimum altitude of 10 000 ft.Most airplanes fly above Mean Sea Level altitudes (MSL), the altimeter would read 5,280 feet in Denver. They are corrected for barometric pressure. When flying above 18,000 feet in the U.S., airplanes express altitude in terms of Flight Levels, which have a standard altimeter setting of 29.92 inches of Mercury.Correct answers: 2 question: A passenger in an airplane flying at an altitude of 37,000 feet sees two towns directly to the west of the airplane. The angles of depression to the towns are 32 degrees nd 76 degrees How far apart are the towns? Round to the nearest mile. (1 mile = 5280 feet)Let h be the length of the hypotenuse. sin C = Opposite hypotenuse sin 10 0 = 30,000 h = 30,000 sine 10 h = 30,000 0.173648 h = 172,763 feet The missing measure is the length of the hypotenuse and given measure of is 10 0 , then the measure of is 80 0 .Math Advanced Math Q&A Library 8. From an airplane which is flying at an altitude of 3000 feet, the angle of depression of an airport ground signal is 27 degrees. Find to the nearest hundred feet the distance between the airplane and the airport signal.= molar mass of Earth's air = 0.0289644 [kg/mol] Earth's Atmosphere Due to the fact that Earth's atmosphere experiences different rates of heating and cooling through each of its layers, these equations help to model this through the use of the temperature lapse rate, which is the rate at which temperature changes through altitude change....auto loan for bad credit

Because the speed of sound increases with air temperature, and air temperature generally decreases with altitude, the true airspeed for a given Mach number generally decreases with altitude. As an airplane moves through the air faster, the airflow over parts of the wing will reach speeds that approach Mach 1.0. 32.0 m: 246 t: Heaviest until the An-22, Mach 3 prototype bomber Antonov An-22: 27 Feb 1965: Transport: 68: 57.9 m: 64.4 m: 250 t: 80 t: Heaviest until the C-5, Heaviest turboprop aircraft Caspian Sea Monster: 16 Oct 1966: Ekranoplan: 1: 92 m: 37.6 m: 544 t: Longest flying vehicle and heaviest until the An-225, crashed in 1980 Lockheed C-5 ... An airplane is flying at an altitude of 33,000 feet. It needs to reduce its altitude by 6% to avoid some turbulence. After it passes the turbulence, it increases its altitude by 5000 feet. What is the final altitude of the airplane? Enter your answer in the box. Advertisement Answer 5.0 /5 7 reinhard10158 Step-by-step explanation: 100% = 33,000 ftSolve the problem.A formula for calculating the distance, d, one can see from an airplane to the horizon on a clear day is where x is the altitude of the plane in feet and d is given in miles. How far can one see in a plane flying at 20,000 feet? Round your answer to the nearest tenth mile, if necessary.Collision between a vulture and an aircraft at an altitude of 37,000 feet.-On 29 November 1973, a Riippell's Griffon (Gyps rueppellii) collided with commercial aircraft at 37,000 ft over Abijan, Ivory Coast, western Africa. The altitude is that recordedWhich is all a roundabout way of explaining that if this plane was flying at 29,000 feet an hour after departure, it was probably just the first step in its pre-programmed series of staggered cruise altitudes, based on fuel, passenger and cargo loads, econ cruise speeds at altitude, winds, etc. as computed by the FMC.But as power drops off, aircraft fly slower, and with stall speeds increasing with altitude, the spread between stall and maximum mach can be very small. That was the case with early Learjets. The closer to stall, the higher your wing angle to your flight path, and that increases drag, so sometimes a lower altitude is more fuel efficient.10. An airplane flying 390 feet per second at an altitude of 5000 feet flew directly over an observer. The image shows the relationship of the airplane to the observer at a later time. a.) Find an equation relating x and y. 5000t 390 ce Б000 b.) Find the value of x when y is 6,250. Observer c.)According to these definitions the transition layer is 0-500 feet (0-152 m) thick. Aircraft are not normally assigned to fly at the "'transition level'" as this would provide inadequate separation from traffic flying on QNH at the transition altitude. Instead, the lowest usable "'flight level'" is the transition level plus 500 ft....nina siemaszko