Sep 10

Space Rocket History #129 – Apollo Mission Control: An Introduction to Eugene Frances Kranz

As Procedures Officer, Kranz was put in charge of integrating Mercury Control with the Launch Control Team at Cape Canaveral, Florida, writing the “Go/NoGo” procedures that allowed missions to continue as planned or be aborted, along with serving as a sort of switchboard operator using teletype between the control center at Cape Canaveral and the agency’s fourteen tracking stations and two tracking ships located across the globe.

Kranz & his F86 Saber Cat

Kranz & his F86 Saber Cat

Kranz at his console in 1965

Kranz at his console in 1965

Kranz and his teacher Chris Kraft

Kranz and his teacher Chris Kraft

Sep 03

Space Rocket History #128 – Apollo Mission Control: Christopher Columbus Kraft – Part 2

At the beginning of the Apollo program, Kraft retired as a flight director to concentrate on management and mission planning. In 1972, he became director of the Manned Spacecraft Center, following the path of his mentor Robert Gilruth.

Kraft in Mission Control for Gemini 5

Kraft in Mission Control for Gemini 5

Ad. Abhau, Robert Thompson, and Kraft

Ad. Abhau, Robert Thompson, and Kraft

Kraft with his new flight Directors

Kraft with his new flight Directors

Aug 27

Space Rocket History #127 – Apollo Mission Control: Christopher Columbus Kraft – Part 1

Christopher Columbus Kraft Jr. was Born on February 28, 1924 in a town that no longer exist, Phoebus, Virginia. The town has now been engulfed by Hampton, Virginia. Kraft was named after his father, Christopher Columbus Kraft, who was born in New York City in 1892 near Columbus Circle at 8th ave. and 59th street.

Chris Kraft & Robert Gilruth

Chris Kraft & Robert Gilruth

Chris Kraft & Wally Schirra

Chris Kraft & Wally Schirra

Kraft at his Mercury Console

Kraft at his Mercury Console

Aug 20

Space Rocket History #126 – Apollo-Saturn IB: AS-201, AS-202, and AS-203

Apollo Saturn 201 employed the Saturn IB launch vehicle, which  was the up-rated version of the Saturn I rocket flown in ten earlier Saturn-Apollo missions. It featured an upgrade of the first stage engines to increase thrust from 1,500,000 lb-ft of thrust to 1,600,000 lb-ft. The second stage was the S-IVB.  This stage used a new liquid hydrogen-burning J-2 engine which would also be used on the S-II second stage of the Saturn V lunar launch vehicle…

AS-201 Recovery

AS-201 Recovery

Apollo-Saturn 201 Launch

Apollo-Saturn 201 Launch

AS-202 Launch

AS-202 Launch

AS-203 Launch

AS-203 Launch