Daily Archives: November 9, 2018

9 November 1967: Air Force Cross, Sergeant Larry Wayne Maysey, United States Air Force

"That Others May Live." Bronze sculpture of Sergeant Larry Wayne Maysey, United States Air Force, by Wayne Hyde. The memorial is located on Main Street, Borough of Chester, New Jersey. (© Sheena Chi)
“That Others May Live.” Bronze statue of Sergeant Larry Wayne Maysey, United States Air Force, by Wayne Hyde. The memorial is located on Main Street, Borough of Chester, New Jersey. (© Sheena Chi)

 AIR FORCE CROSS

Awarded posthumously for actions during the Vietnam War

Sgt. Larry W. Masey
Sergeant Larry W. Maysey, Rescue Specialist, United States Air Force

The President of the United States of America, authorized by Title 10, Section 8742, United States Code, takes pride in presenting the Air Force Cross (Posthumously) to Sergeant Larry Wayne Maysey (AFSN: 12751422), United States Air Force, for extraordinary heroism in connection with military operations against an opposing armed force as an HH-3E Rescue Specialist (Pararescueman) of the 37th Aerospace Rescue and Recovery Squadron, 3d Air Rescue and Recovery Group, DaNang Air Base, Vietnam, in Southeast Asia on 9 November 1967. On that date, Sergeant Maysey attempted the night extraction of a ground reconnaissance team after his helicopter had been severely damaged. Two other helicopters had been shot down and a third extensively damaged in previous attempts. During the rescue attempt, Sergeant Maysey unhesitatingly exposed himself to the hail of hostile fire to assist wounded survivors into the helicopter. The hostile forces closed in quickly, and as the damaged helicopter departed, it was shot down. Though his extraordinary heroism, superb airmanship, and aggressiveness in the face of the enemy, Sergeant Maysey reflected the highest credit upon himself and the United States Air Force.

Action Date: 9-Nov-67

Service: Air Force

Rank: Sergeant

Company: 37th Aerospace Rescue and Recovery Squadron

Regiment: 3d Air Rescue and Recovery Group

Division: DaNang Air Base, Vietnam

Air Force Cross
Air Force Cross

Larry Wayne Maysey was born 18 November 1946 in the Borough of Chester, new jersey. he was the son of Charles and Charlotte Maysey. He attended West Morris High School, graduating in 1965.

After graduating from high school, Larry Maysey enlisted in the United States Air Force, and was selected for training as a Pararescue Jumper at Lackland Air Force Base, Texas. The “PJs” of the U.S. Air Force are graduates of an two-year training course, known as “the Pipeline,” which is one of the most intense training programs of any military service. The failure rate is about 80%.

Sergeant Maysey arrived in Vietnam in mid-October 1967, assigned to the 37th Aerospace Rescue and Recovery Squadron. On 9 November 1967, he was one of the crew of “Jolly Green 26,” A Sikorsky HH-3E Jolly Green Giant Combat Search and Rescue (CSAR) helicopter.

Sergeant Maysey’s remains were not recovered. His name is inscribed on the Courts of the Missing, at the Honolulu Memorial, National Memorial Cemetery of the Pacific.

© 2017, Bryan R. Swopes

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9 November 1967: Air Force Cross, Staff Sergeant Eugene Lunsford Clay, United States Air Force

Air Force Cross
Eugene Lunsford Clay

The President of the United States of America, authorized by Title 10, Section 8742, United States Code, takes pride in presenting the Air Force Cross (Posthumously) to Staff Sergeant Eugene Lunsford Clay (AFSN: 18497841), United States Air Force, for extraordinary heroism in connection with military operations against an opposing armed force as an HH-3E Flight Engineer of the 37th Aerospace Rescue and Recovery Squadron, 3d Air Rescue and Recovery Group, DaNang Air Base, Vietnam, in action in Southeast Asia on 9 November 1967. On that date, Sergeant Clay attempted the night extraction of a ground reconnaissance team after his helicopter had been severely damaged. Two other helicopters had been shot down and a third extensively damaged in previous attempts. During the rescue attempt, Sergeant Clay unhesitatingly exposed himself to hostile fire to assist the survivors to the aircraft. The hostile forces closed in quickly, and as the damaged helicopter departed, it was shot down. Through his extraordinary heroism, superb airmanship, and aggressiveness in the face of hostile forces, Staff Sergeant Clay reflected the highest credit upon himself and the United States Air Force.

Action Date: November 9, 1967

Service: Air Force

Battalion: 37th Aerospace Rescue and Recovery Squadron

Regiment: 3d Air Rescue and Recovery Group

Division: DaNang Air Base, Vietnam

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9 November 1967: Air Force Cross, Captain Ralph Wayne Brower, United States Air Force Reserve

Air Force Cross
Ralph Wayne Brower

The President of the United States of America, authorized by Title 10, Section 8742, United States Code, takes pride in presenting the Air Force Cross (Posthumously) to Captain Ralph Wayne Brower (AFSN: 0-3109303), United States Air Force (Reserve), for extraordinary heroism in connection with military operations against an opposing armed force as an HH-3E pilot of the 37th Aero Space Rescue and Recovery Squadron, 3d Air Rescue and Recovery Group, DaNang Air Base, Vietnam, in action in Southeast Asia on 9 November 1967. On that date, captain Brower attempted the night extraction of a ground reconnaissance team. Despite full knowledge that two helicopters had been shot down and a third severely damaged by intense, accurately directed hostile fire, Captain Brower, with determination, indomitable courage, and profession skill, established a hover on a steep slope within one hundred yards of hostile weapons positions and brought the wounded survivors aboard. The hostile forces closed in quickly, and as the helicopter departed, it was shot down. Through his extraordinary heroism, superb airmanship, and aggressiveness in the face of hostile forces, Captain Brower reflected the highest credit upon himself and the United States Air Force.

Action Date: November 9, 1967

Service: Air Force

Battalion: 37th Aerospace Rescue and Recovery Squadron

Regiment: 3d Air Rescue and Recovery Group

Division: DaNang Air Base, Vietnam

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9 November 1967: Medal of Honor, Captain Gerald Orren Young, United States Air Force

Medal of Honor

MEDAL OF HONOR

YOUNG, GERALD O.

Lieutenant Colonel Gerald Orren Young, United States Air Force. (1930–1990)

Rank and organization: Captain, U.S. Air Force, 37th ARS Da Nang AFB, Republic of Vietnam.

Place and date: Khesanh, 9 November 1967.

Entered service at: Colorado Springs, Colo. Born: 9 May 1930, Chicago, Ill.

Citation: For conspicuous gallantry and intrepidity at the risk of his life above and beyond the call of duty. Capt. Young distinguished himself while serving as a helicopter rescue crew commander. Capt. Young was flying escort for another helicopter attempting the night rescue of an Army ground reconnaissance team in imminent danger of death or capture. Previous attempts had resulted in the loss of 2 helicopters to hostile ground fire. The endangered team was positioned on the side of a steep slope which required unusual airmanship on the part of Capt. Young to effect pickup. Heavy automatic weapons fire from the surrounding enemy severely damaged 1 rescue helicopter, but it was able to extract 3 of the team. The commander of this aircraft recommended to Capt. Young that further rescue attempts be abandoned because it was not possible to suppress the concentrated fire from enemy automatic weapons. With full knowledge of the danger involved, and the fact that supporting helicopter gunships were low on fuel and ordnance, Capt. Young hovered under intense fire until the remaining survivors were aboard. As he maneuvered the aircraft for takeoff, the enemy appeared at point-blank range and raked the aircraft with automatic weapons fire. The aircraft crashed, inverted, and burst into flames. Capt. Young escaped through a window of the burning aircraft. Disregarding serious burns, Capt. Young aided one of the wounded men and attempted to lead the hostile forces away from his position. Later, despite intense pain from his burns, he declined to accept rescue because he had observed hostile forces setting up automatic weapons positions to entrap any rescue aircraft. For more than 17 hours he evaded the enemy until rescue aircraft could be brought into the area. Through his extraordinary heroism, aggressiveness, and concern for his fellow man, Capt. Young reflected the highest credit upon himself, the U.S. Air Force, and the Armed Forces of his country.

Sikorsky HH-3E 66-13290, a Jolly Green Giant rescue helicopter of the 37th Air Rescue Squadron, Da Nang, Republic of Vietnam, 1968. This aircraft is similar to 66-13279, Jolly Green 26, the helicopter flown by Captain Young, 9 November 1967. (U.S. Air Force)
Sikorsky HH-3E Sea King 66-13290, a “Jolly Green Giant” rescue helicopter of the 37th Air Rescue Squadron, Da Nang, Republic of Vietnam, 1968. This aircraft the same type as 66-13279, “Jolly 26,” the helicopter flown by Captains Young and Brower, 9 November 1967. (U.S. Air Force)

The remaining crew members of Jolly Green 26 died in the crash. They were Captain Ralph Wayne Brower, the helicopter’s co-pilot; Staff Sergeant Eugene Lunsford Clay, flight engineer; Sergeant Larry Wayne Maysey, Pararescueman. The soldiers that “Jolly 26” had just rescued, Special Forces Master Sergeant Bruce Raymond Baxter and Specialist 4 Joseph George Kusick, both of U.S. Army Reconnaissance Team UTAH, were also killed.

Captain Brower, Staff Sergeant Clay and Sergeant Maysey were each posthumously awarded the Air Force Cross for “extraordinary heroism” during the rescue.

Hill 891, a 2,923-foot hilltop just west of the Laos/Vietnam Border: the crash site of UH-1D "Spartan 53" and HH-3E "Jolly Green 26," 9 November 1967. (190th AHC)
Hill 891, a 2,923-foot hilltop just west of the village of Talat Luay, Laos, near the Vietnam Border: the crash site of UH-1D “Spartan 53” and HH-3E “Jolly Green 26,” 9 November 1967. (190th AHC)

The Sikorsky HH-3E (Sikorsky S-61R) earned the nickname Jolly Green Giant during the Vietnam War. It is a dedicated Combat Search and Rescue (CSAR) helicopter flown by the U.S. Air Force, based on the CH-3C transport helicopter. The aircraft is flown by two pilots and the crew includes a flight mechanic and gunner. It is a large twin-engine helicopter with a single main rotor/tail rotor configuration. It has retractable tricycle landing gear and a rear cargo ramp. The rear landing gear retracts into a stub wing on the aft fuselage. The helicopter has an extendable inflight refueling boom.

The HH-3E is 72 feet, 7 inches (22.123 meters) long and 18 feet, 10 inches (5.740 meters) high with all rotors turning. The main rotor has five blades and a diameter of 62 feet (18.898 meters). Each blade has a chord of 1 foot, 6.25 inches (0.464 meters). The main rotor turns at 203 r.p.m., counter-clockwise, as seen from above. (The advancing blade is on the right.) The tail rotor also has five blades and has a diameter of 10 feet, 4 inches (3.150 meters). The blades have a chord of 7–11/32 inches (0.187 meters). The tail rotor turns clockwise as seen from the helicopter’s left. (The advancing blade is below the axis of rotation.) The tail rotor turns 1,244 r.p.m.

The HH-3E has an empty weight of 13,341 pounds (6,051 kilograms). The maximum gross weight is 22,050 pounds (10,002 kilograms).

The Jolly Green Giant is powered by two General Electric T58-GE-5 turboshaft engines, which have a Maximum Continuous Power rating of 1,400 shaft horsepower, each, and Military Power rating of 1,500 shaft horsepower. The main transmission is rated for 2,500 horsepower, maximum.

The HH-3E has a cruise speed of 154 miles per hour (248 kilometers per hour) at Sea Level, and a maximum speed of 177 miles per hour (285 kilometers per hour), also at Sea Level. The service ceiling is 14,000 feet (4,267 meters). The HH-3E had a maximum range of 779 miles (1,254 kilometers) with external fuel tanks.

The Jolly Green Giant can be armed with two M60 7.62 mm machine guns.

Sikorsky built 14 HH-3Es. Many CH-3Cs and CH-3Es were upgraded to the HH-3E configuration. Sikorsky built a total of 173 of the S-61R series.

Sikorsky HH-3E Jolly Green Giant 67-14709 at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force)

© 2018, Bryan R. Swopes

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9 November 1967, 12:00:01.263 UTC, T plus 0.263

Apollo 4 Saturn V (AS-501) on the launch pad at sunset, the evening before launch, 8 November 1967. (NASA)
Apollo 4 Saturn V (AS-501) on the launch pad at sunset, the evening before launch, 8 November 1967. (NASA)

9 November 1967: The first flight of a Saturn V took place when the unmanned Apollo 4/Saturn V (AS-501) was launched from Pad 39A at the Kennedy Space Center, Cape Canaveral, Florida. The rocket lifted off at 12:00:01.263 UTC.

AS-501 consisted of the first Saturn V launch vehicle, SA-501, with Apollo Spacecraft 017 (a Block I vehicle with Block II upgrades), and included the Launch Escape Tower, Command Module, Service Module, Lunar Module Adapter, and Lunar Module Test Article LTA-10R).

The Saturn V rocket was a three-stage, liquid-fueled heavy launch vehicle. Fully assembled with the Apollo Command and Service Module, it stood 363 feet, 0.15 inches (110.64621 meters) tall, from the tip of the escape tower to the bottom of the F-1 engines. The first and second stages were 33 feet, 1.2 inches (10.089 meters) in diameter. Fully loaded and fueled the rocket weighed 6,200,000 pounds (2,948,350 kilograms).¹ It could lift a payload of 260,000 pounds (117,934 kilograms) to Low Earth Orbit.

The first stage was designated S-IC. It was designed to lift the entire rocket to an altitude of 220,000 feet (67,056 meters) and accelerate to a speed of more than 5,100 miles per hour (8,280 kilometers per hour). The S-IC stage was built by Boeing at the Michoud Assembly Facility, New Orleans, Louisiana. It was 138 feet (42.062 meters) tall and had an empty weight of 290,000 pounds (131,542 kilograms). Fully fueled with 203,400 gallons (770,000 liters) of RP-1 and 318,065 gallons (1,204,000 liters) of liquid oxygen, the stage weighed 5,100,000 pounds (2,131,322 kilograms). It was propelled by five Rocketdyne F-1 engines, producing 1,522,000 pounds of thrust, each, for a total of 7,610,000 pounds of thrust at Sea Level.² These engines were ignited seven seconds prior to lift off and the outer four burned for 168 seconds. The center engine was shut down after 142 seconds to reduce the rate of acceleration. The F-1 engines were built by the Rocketdyne Division of North American Aviation at Canoga Park, California.

A Rocketdyne F-1 engine is being installed on a Saturn S-IC first stage. (NASA)

The S-II second stage was built by North American Aviation at Seal Beach, California. It was 81 feet, 7 inches (24.87 meters) tall and had the same diameter as the first stage. The second stage weighed 80,000 pounds (36,000 kilograms) empty and 1,060,000 pounds loaded. The propellant for the S-II was liquid hydrogen and liquid oxygen. The stage was powered by five Rocketdyne J-2 engines, also built at Canoga Park. Each engine produced 232,250 pounds of thrust, and combined, 1,161,250 pounds of thrust.³

The Saturn V third stage was designated S-IVB. It was built by Douglas Aircraft Company at Huntington Beach, California. The S-IVB was 58 feet, 7 inches (17.86 meters) tall with a diameter of 21 feet, 8 inches (6.604 meters). It had a dry weight of 23,000 pounds (10,000 kilograms) and fully fueled weighed 262,000 pounds. The third stage had one J-2 engine and also used liquid hydrogen and liquid oxygen for propellant.⁴ The S-IVB would place the Command and Service Module into Low Earth Orbit, then, when all was ready, the J-2 would be restarted for the Trans Lunar Injection.

Eighteen Saturn V rockets were built. They were the most powerful machines ever built by man.

Apollo 4 Saturn V AS-501 lifts off at 12:00:01 UTC, 9 November 1967. (NASA)
Apollo 4 Saturn V (AS-501) lifts off at 12:00:01 UTC, 9 November 1967. (NASA)

¹ The AS-501 total vehicle mass at First Motion was 6,137,868 pounds (2,784,090 kilograms).

²  Post-flight analysis gave the total thrust of AS-501’s S-IC stage as 7,728,734.5 pounds of thrust (34,379.1 kilonewtons).

³ Post-flight analysis gave the total thrust of AS-501’s S-II stage as 1,086,396 pounds of thrust (4,832.5 kilonewtons).

⁴ Post-flight analysis gave the total thrust of AS-501’s S-IVB stage as 222,384 pounds of thrust (989.2 kilonewtons) during the first burn; 224,001 pounds (996.4 kilonewtons) during the second burn.

© 2017, Bryan R. Swopes

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