
20 July 1969, 18:12:01 UTC, T + 100 hours, 40 minutes, 1.9 seconds: The Lunar Module Eagle completes the separation maneuver, moving away from the Apollo 11 Command and Service Module Columbia.
© 2015, Bryan R. Swopes
20 July 1969, 18:12:01 UTC, T + 100 hours, 40 minutes, 1.9 seconds: The Lunar Module Eagle completes the separation maneuver, moving away from the Apollo 11 Command and Service Module Columbia.
© 2015, Bryan R. Swopes
In the late 1940s engineers began working on an aircraft that could be powered by a nuclear reactor. The reactor would heat air to provide jet thrust, rather than burning fuel and air to do so. A 60 megawatt reactor was envisioned.
The NB-36 was built to test the shielding requirements of an airborne nuclear reactor and to determine the effects of radiation on aircraft systems.
The Nuclear Test Aircraft was built from a Convair B-36H-20-CF Peacemaker strategic bomber, one of 61 that had been destroyed or damaged by a tornado that struck Carswell AFB in 1952. 51-5712 was so heavily damaged that the airframe was written off, but it was rebuilt with a completely new nose section with a shielded cockpit, and was otherwise very heavily modified by Convair. Originally designated XB-36H-20-CF, this was changed to NB-36H in June 1956.
As with other B-36s, a combination of six Pratt & Whitney Wasp Major R-4360-53 air-cooled, 28-cylinder radial engines, and four General Electric J47-GE-19 turbojet engines, powered the NB-36.
The modified bomber could reach a maximum speed of 420 miles per hours at 47,000 feet. It had a maximum gross weight of 357,500 pounds.
During the test program, the NB-36 made 47 flights with a total of 215 hours flight time.
Based on the test results, the entire project was cancelled, and 51-5712 was scrapped at Fort Worth in 1958.
© 2016, Bryan R. Swopes
20 July 1933: At 11:58 a.m. (17:58 UTC) on the fifth day of his solo around-the-world flight, Wiley Post took off from Khabarovsk, Siberia, heading toward Nome, Alaska, 2,416 miles (3,888 kilometers) to the east-northeast (great circle route).
Post missed his destination and, exhausted, became lost. He flew over Alaska for approximately seven hours before sighting a remote U.S. Army Signal Corps radio station at Flat, Alaska, a small gold mining town located along the Iditarod Trail in southwestern Alaska.
Post landed his Lockheed Model 5C Vega, NR105W, The Winnie Mae of Oklahoma, on a small landing field at the eastern edge of the town. The airplane’s wheels sank into the soft surface and Winnie Mae nosed over, damaging its propeller, engine cowling and right landing gear strut. Wiley Post was unhurt.
The International News Service (INS) reported:
. . . Utter exhaustion which numbed his mind so that he could not properly pilot his course caused him to become lost for seven hours over Alaska yesterday after he had been in the air more than 22 hours on his 3,000-mile hop from Siberia to Alaska during which he battled the most adverse weather conditions, he revealed today.
Sighting the Flat radio station caused him to land here. He said that he could at least get his directions again. He ran into soft ground on the landing field, nosing over, breaking his right wheel strut, damaging the engine cowling and valves and bending the propeller. Post was uninjured. . . .
A replacement propeller was flown in from Fairbanks and repairs were made. He continued the following day, taking off at 7:28 a.m., local.
© 2016, Bryan R. Swopes
At 3:16:10 p.m., the fan disk of the airliner’s tail-mounted General Electric CF6-6 turbofan engine (Number Two) failed catastrophically. Shrapnel from the exploding engine chopped through the DC-10’s tail section and severed the three independent hydraulic systems that powered the flight control surfaces. The crew immediately lost their ability to control the airliner with rudder, elevators and ailerons. Flaps and wing leading edge slats were inoperative. Controls to the damaged engine also failed and only by cutting off fuel flow were they able to shut if down and prevention further damage or a fire. Landing gear could only be lowered by use of an emergency procedure.
The uncontrolled airliner immediately started to roll and dive. The pilots’ cockpit flight controls were completely useless to stop the roll. Only by varying the thrust on the two remaining wing mounted engines could some degree of control be maintained. Realizing there was a problem with the DC-10, Captain Fitch told a flight attendant to inform Captain Haynes that he was aboard and ask if he could assist. Haynes immediately asked Fitch to come forward, and once there to take over the throttle controls while the crew dealt with all the other problems that were occurring.
The simultaneous loss of all three hydraulic systems was considered to be “impossible” and there were no emergency procedures to deal with the problem. The crew did the best they could by varying power on the two remaining engines to turn the airplane and to descend. They were heading for an emergency landing at Sioux City Gateway Airport, Iowa (SUX).
At 4:00:16 p.m., the DC-10 touched down on Runway 22 at an estimated at 215 knots (247.4 miles per hour, 398.2 kilometers per hour) and a rate of descent of 1,620 feet per minute (8.23 meters per second). At about 100 feet (30.5 meters) above the ground, the airliner’s nose began to pitch downward and the airliner started to roll to the right. Touchdown was at the runway threshold, just left of the centerline.
The force of the impact caused the airframe break apart and the wreck rolled over to the right side of the runway. Fuel exploded and fire spread. 110 passengers and 1 flight attendant were killed in the crash and fire. There were 185 survivors of the crash, including the four pilots who were trapped in the crushed nose section of the airplane which had broken away from the main wreckage.
The National Transportation Safety Board (NTSB) investigation determined that the the center engine fan disk failed due to a crack which had formed when the original titanium ingot from which it was made had been cast 18 years before.
The official report said that a landing under these conditions was stated to be “a highly random event“. The NTSB further noted that “. . . under the circumstances the UAL flight crew performance was highly commendable and greatly exceeded reasonable expectations.”
This was one of the finest displays of airmanship during an inflight emergency since the beginning of aviation.
© 2018, Bryan R. Swopes
19 July 1969, 22:42 UTC, T + 81 hours, 10 minutes: Just over 58 minutes since the Apollo 11 spacecraft entered a circular orbit around the Moon, Lunar Module Pilot (LMP) Edwin E. “Buzz” Aldrin entered the Lunar Module Eagle to power it up and start systems checks in preparation for the descent to the Lunar surface.
© 2015, Bryan R. Swopes