Skylab was an orbital laboratory built from a Saturn S-IVB third stage. It was launched from Cape Canaveral 14 May 1973 as part of a modified Saturn V rocket. The Skylab 4 crew was the third and final group of astronauts to live and the space station. (The mission insignia incorporates the numeral 3.)
Skylab’s orbit gradually decayed and it re-entered the atmosphere near Perth, Australia, 11 July 1979.
© 2019, Bryan R. Swopes
This was a new Fédération Aéronautique Internationale (FAI) world distance record for turboprop airplanes.¹ The Orion’s course deviated around foreign airspace so the actual distance flown was 7,010 miles (11,218.5 kilometers).
For the long distance flight the Orion carried a flight crew of seven: Commander Donald H. Lilienthal, Aircraft Commander; Captain R.H. Ross, Pilot; Lieutenant Commander F. Howard Stoodley, Pilot; Lieutenant R.T. Myers, Navigator; Commander J.E. Koehr, Meteorologist; Chief Aviation Machinist’s Mate K.D. Frantz, Flight Engineer; and Chief Aviation Electrician’s Mate H.A. Statti, Flight Engineer.
On Wednesday, 27 January 1971, the same airplane set both FAI and National Aeronautic Association records for Speed Over a Straight Course of 15/25 Kilometers of 806.10 kilometers per hour (500.89 miles per hour) at NAS Patuxent River.²
The U.S. National Record still stands:
On February 4, at Edwards Air Force Base in the high desert of Southern California, Commander Lilienthal flew 156512 to a World Record for Altitude in Horizontal Flight of 13,721.5 meters (45,018.1 feet).³
On 8 February 1971, while till at Edwards AFB, Commander Lilienthal and 156512 set five more world records for heavy turboprop airplanes. The P-3C climbed to a height of 3,000 meters (9,843 feet) in 2 minutes, 52 seconds ⁴ ; to 6,000 meters (19,685 feet) in 5 minutes, 46 seconds ⁵ ; to 9,000 meters (29, 528 feet) in 10 minutes, 26 seconds ⁶ ; and 12,000 meters (39,370 feet) in 19 minutes, 42 seconds.⁷ The Orion continued climbing until it reached a world record altitude of 14,086.1 meters (46,214.2 feet). ⁸
For his record-setting flights, Commander Lilienthal was awarded the Distinguished Flying Cross.
The Lockheed P-3 Orion was developed from the Model 188 Electra—a four-engine turboprop airliner which first flew in 1957—primarily as a long-range anti-submarine warfare and maritime surveillance aircraft. The P-3 has been adapted to many other missions. The P-3C variant in U.S. Navy service is usually operated by a crew of 11.
The bomber is 116 feet, 10 inches (35.611 meters) long with a wingspan of 99 feet, 8 inches (30.378 meters) and overall height of 34 feet, 3 inches (10.439 meters). It has a zero-fuel weight of 77,200 pounds (35,017 kilograms) and a normal maximum takeoff weight of 135,000 pounds (61,235 kilograms) (Overload Takeoff: 139,780 pounds/63,403 kilograms).
The P-3C can remain airborne for 16 hours.
There is a wide variety of sensors board the P-3. Sonobuoys can be dropped from the belly. A Magnetic Anomaly Detector, the “MAD boom” is mounted at the tail of the aircraft.
The Orion caries no defensive weapons. It can carry bombs, depth charges, torpedoes, mines, air-to-surface and anti-ship missiles, and nuclear weapons.
More than 750 P-3 Orions and its variants were built by Lockheed and licensee Kawasaki Heavy Industries between 1961 and 1996. In addition to the U.S. Navy and various Federal government agencies, the Lockheed P-3 Orion remains in service worldwide with more than twenty countries.
Lockheed P-3C-110-LO Orion Bu. No. 156512 served as a test aircraft at Patuxent River until 15 July 1974. It was then assigned to VP-31 where it remained for over nine years, carrying the squadron identification marking RP and the numeral 9. It later served with VP-9, VP-46, VP-65, VP-16 and finally, VP-45. 156512 was placed in long-term storage at Davis-Monthan Air Force Base, Tucson, Arizona, in 1995, and was scrapped in 2004.
Donald Herman Lilienthal was born 6 February 1931 at Pope, Minnesota. He was the fourth child of Frederick R. Lilienthal, a steam railway worker, and Bertha Camille Metlie Lilienthal. He attended Glenwood High School, Glenwood, Minnesota, graduating in 1949. He then studied mathematics at the University of Minnesota, before accepting an appointment as a midshipman at the United States Naval Academy at Annapolis, Maryland, in 1951.
Midshipman Lilienthal graduated from Annapolis and was commissioned an ensign, United States Navy, 3 June 1955. He was then trained as a pilot. Later, he graduated from the United States Naval Test Pilot School at NAS Patuxent River, Maryland.
In June 1958, Lieutenant (j.g.) Lilienthal married Miss Jeanne L. Murphy, in Duval County, Florida. They had three children, Karen, John and Donald, Jr. They divorced in March 1975.
Lieutenant (j.g.) Lilienthal was promoted to the rank of lieutenant 1 July 1959, and to lieutenant commander, 1 July 1964. He advanced to commander on 1 July 1969.
Commander Lilenthal retired from the United States Navy in December 1975 after 20 years of service as an antisubmarine warfare pilot and test pilot. He later worked as a consultant to the aviation industry.
Commander Lilienthal married Mrs. Jimena Rosa Goich Recavrren, a widow, in Arlington, Virginia, 17 September 1982. They divorced 3 December 1993 in Fairfax, Virginia.
Commander Donald Herman Lilienthal, United States Navy (Retired) passed away at Loudon, Virginia, 21 August 2014 at the age of 83 years. He is buried at Arlington National Cemetery, Arlington, Virginia.
¹ FAI Record File Number 8070
² FAI Record File Number 8582
³ FAI Record File Number 8476
⁴ FAI Record File Number 3400
⁵ FAI Record File Number 3401
⁶ FAI Record File Number 3402
⁷ FAI Record File Number 3403
⁸ FAI Record File Number 8055
© 2019, Bryan R. Swopes
8 February 1949: One of the two Boeing XB-47 Stratojet prototypes made a record-breaking transcontinental flight from Moses Lake Air Force Base, Washington, to Andrews Air Force Base, Maryland, in 3 hours, 46 minutes. The XB-47 departed Moses Lake at 10:22 a.m., Eastern Standard Time (15:22 UTC), and crossed over the Andrews Field control tower at 13,000 feet (3,962 meters) at 2:08 p.m. (19:08 UTC). Majors Russell Ellsworth (“Russ”) Schleeh and Joseph Woodrow Howell beat the official U.S. national record set two years earlier by Colonel William Haldane Councill in a specially-prepared Lockheed P-80A Shooting Star.¹
Major Schleeh was the Deputy Chief of Bomber Operations in the Flight Test Division of the Air Material Command, Wright-Patterson Air Force Base, Dayton, Ohio.
The Los Angeles Times reported:
Jet Bomber Spans Nation in 3 Hours 46 Minutes
New Plane Averages 607.2 m.p.h. to Make Fastest Coast-to-Coast Journey on Record
Washington, Feb. 8 (AP)—An arrow-shaped XB-47 jet bomber streaked through the stratosphere at an average speed of 607.2 miles an hour today in the fastest transcontinental flight ever made.
The bomber, rated as “light” despite its 125,000 pounds, flew 2289 miles from Moses Lake (Wash.) Air Base to Andrews Field, Md., a few miles south of the capital, in 3h. 46m.
The pace was 27 minutes shorter in time and 23 miles faster in average speed than the official record of 4h. 13m. at 584 m.p.h. established by Col. William H. Council [sic] in an F-80 Shooting Star two years ago.
No Official Claim
However, the Air Force will claim no record. The flight was not timed officially and it did not fly the recognized contest course. The recognized course—the one Col. Council flew—is Los Angeles to new York, 2464 miles.
The XB-47 is a six-engine, swept wing bomber built by Boeing Airplane Co. at Seattle, known as the Stratojet, it is the Air Force’s first bomber designed for speeds in excess of 600 miles an hour.
The XB-47 is the plane to which Air Force Secretary Symington referred last fall when he mentioned a jet bomber running away from jet fighters. Ten XB-47s are to be built at Boeing’s Wichita (Kan.) plant, where about half of all the B-29s were built during the war.
Maj. Russell E. Schleeh, pilot, and Maj. Joseph W. Howell, co-pilot, both said the flight was strictly routine. They were comfortable in a new type flying suit being tested by the Materiel Command, used oxygen all the way, and navigated by radio compass on a great circle course which took them 20 miles south of Chicago.
The first part of the flight was at 32,000 feet. Later they moved up to 37,000 feet. The pressurized cabin was maintained at 23,000 feet. During one hour they covered 648 miles.
In addition to six J-35 turbo-jet engines built by General Electric Co. at Lynn, Mass., which gave a total of 24,000 pounds of thrust, the Stratojet can use 18 rockets each capable of delivering 1000 pounds of thrust for a few seconds. The rockets were not carried today.
The XB-47 carries a parachute in its tail to help it stop quickly.
—Los Angeles Times, Vol. LXVIII, 9 February 1949, Page 1, Columns 6 and 7, and Page 3, Columns 1–8
Designed as a strategic bomber, the B-47 could fly higher and faster than jet fighters of the time, and it was also highly maneuverable. The XB-47 (Boeing Model 450) was flown by a two-man crew in a tandem cockpit. It was 107 feet, 6 inches (32.766 meters) long with a wingspan of 116 feet (35.357 meters). The top of the vertical fin was 27 feet, 8 inches (8.433 meters) high. The wings were shoulder-mounted with the leading edges swept at 35°.
The first prototype, 46-065, was powered by six General Electric J35-GE-7 axial flow turbojet engines in four pods mounted on pylons below the wings. The J35 was a single-spool, axial-flow turbojet engine with an 11-stage compressor and single-stage turbine. The J35-GE-7 was rated at 3,750 pounds of thrust (16.68 kilonewtons) at 7,700 r.p.m. (static thrust, Sea Level). The engine was 14 feet, 0.0 inches (4.267 meters) long, 3 feet, 4.0 inches (1.016 meters) in diameter and weighed 2,400 pounds (1,089 kilograms). (The second prototype, 46-066, was completed with J47 engines. 46-065 was later retrofitted with these engines.)
The XB-47 prototype had a maximum speed of 502 knots (578 miles per hour/930 kilometers per hour/0.80 Mach) at 15,000 feet (4,572 meters). The combat speed was 462 knots (532 miles per hour/856 kilometers per hour/0.70 Mach) at 35,000 feet (10,668 meters). The prototype’s empty weight was 74,623 pounds (33,848 kilograms), while its maximum takeoff weight was 162,500 pounds (73,709 kilograms). It required a ground run of 11,900 feet (3,627 meters), or 4,800 feet (1,463 meters) with JATO assist. The bomber could climb at a rate of 3,650 feet per minute (18.5 meters per second) at Sea Level, at combat weight and maximum power. The service ceiling was 37,500 feet (11,430 meters). The XB-47 carried 9,957 gallons (37,691 liters) of fuel. The combat radius was 1,175 nautical miles (1,352 statute miles/2,176 kilometers) with a 10,000 pound (4,536 kilogram) bomb load.
Planned armament (though the XB-47s were delivered without it) consisted of two .50-caliber machine guns in a tail turret, with 1,200 rounds of ammunition, and 10,000 pounds (4,536 kilograms) of bombs.
The Stratojet was one of the most influential aircraft designs of all time and its legacy can be seen in almost every jet airliner built since the 1950s: the swept wing with engines suspended on pylons, , mounted forward of the leading edge.
2,032 B-47s were built by Boeing Wichita, Douglas Tulsa and Lockheed Marietta. They served the United States Air Force from 1951 to 1977.
The very last B-47 flight took place 18 June 1986 when B-47E-25-DT, serial number 52-166, was flown from the Naval Air Weapons Center China Lake to Castle Air Force Base to be placed on static display.
XB-47 45-065 stalled while landing at Larson Air Force Base, near Moses Lake, Washington, 18 August 1951. The crew of three escaped uninjured. The airplane was damaged beyond repair. The second prototype, XB-47 46-066, is in the collection of the Air Force Flight Test Museum, Edwards Air Force Base, California.
¹ See This Day in Aviation for 26 January 1946 at: https://www.thisdayinaviation.com/26-january-1946/
© 2023, Bryan R. Swopes
The 247 is considered to be the first modern airliner because of its all-metal semi-monocoque construction, cantilevered wing and retractable landing gear. It was 50 miles per hour (80.5 kilometers per hour) faster than its contemporaries, and could climb on one engine with a full load.
The airplane was built at Boeing’s Oxbow factory on the Duwamish River, then barged to Boeing Field where it was assembled and tested. The 247 was originally named “Skymaster,” but this was soon dropped.
Two months after the first flight, the first production 247, NC13301, was placed in service with United Air Lines. It was the first of ten 247s bought by United.
The Model 247 was operated by a pilot, co-pilot and a flight attendant and carried up to ten passengers. The airplane was 51 feet, 5 inches (15.672 meters) long, with a wingspan of 74 feet, 1 inch (22.581 meters) and overall height of 12 feet, 5 inches (3.785 meters). The empty weight was 8,921 pounds (4,046.5 kilograms) with a maximum takeoff weight of 16,805 pounds (7,622.6 kilograms).
The Duralamin skin panels were anodized, rather than painted, for corrosion protection. This saved weight, and resulted in the 247’s characteristic gray-green color.
The Boeing 247 had a maximum speed of 200 miles per hour (321.9 kilometers per hour) with a cruising speed of 188 miles per hour (302.6 kilometers per hour. It had a range of 745 miles (1,199 kilometers) and a service ceiling of 25,400 feet (7,742 meters).
75 Model 247s were built. 60 were bought by Boeing Air Transport.
[Note: the windshield was canted forward to prevent instrument panel lighting from reflecting into the cockpit at night. Unfortunately, ground lighting was reflected instead. This was soon changed to a rearward slant and resulted in a slight increase in speed.]
© 2019, Bryan R. Swopes
8 February 1918: General Order 299 specified that all U.S. Army Air Service airplanes assigned to the AEF would be marked with a roundel (or cocarde) of three concentric circles. The outer circle was to be painted red and have a diameter approximately equal to the chord of the wing. A blue circle had a diameter two-thirds the length of the chord, and an inner white circle was one-third the chord in diameter. Two roundels were painted on the upper surface of the airplane’s top wing, just inside the aileron. Two more roundels were painted on the lower surface of the bottom wing.
In addition the airplane’s rudder was painted with three red, white and blue vertical stripes, with the red stripe adjacent to the rudder post and the blue stripe on the rudder’s trailing edge.
This national insignia was similar to the roundels used by France and England, though the order of the colors varied.
The red, blue and white roundel replaced the previous national insignia, which was a white 5-pointed star surrounded by a blue circle, with a red circle in the center. The star insignia had also been place in the same position on the wings, and the rudder also had three vertical stripes, but the order had been blue, white and red.
The new roundel was short-lived. It was replaced in 1919.
© 2016, Bryan R. Swopes