Tag Archives: Saturn IB

Jul 09

Space Rocket History #120 – Apollo: Stages S-IV and S-IVB

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The key to high-energy stages was to use liquid hydrogen as the fuel.  Liquid hydrogen fuel appealed to rocket designers because of its high specific impulse, which is a basic measure of rocket performance. Specific Impulse is the impulse delivered per unit of propellant consumed.  You might think of it as the efficiency of the rocket.  Compared to an RP-1 (kerosene) fueled engine of similar size, liquid hydrogen fuel could increase the specific impulse or efficiency of an engine by 40 percent.  The combination of hydrogen and oxygen for propellants made the moon shot feasible.

S-IV Rocket Stage

S-IV Rocket Stage

S-IV & S-IVB Stage Position

S-IV & S-IVB Stage Position

S-IV Stage in Saturn IB and V

S-IV Stage in Saturn IB and V

S-IVB Differences Between Saturn IB and V

S-IVB Differences Between Saturn IB and V

May 21

Space Rocket History #114 – Apollo: Command Module Design and Development 1963-1964 Part 2

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Max Faget’s position was that considering the difficulty of the job,  if each mission was successful half the time, it would be well worth the effort.  But Gilruth thought that was too low.  He want a 90% mission success ratio and a 99% ratio for Astronaut safety.  Walt Williams who was currently running the Mercury program believed that astronaut safety needed to be limited to only 1 failure in a million which was 99.9999%.

Launch Escape Vehicle Configuration

Launch Escape Vehicle Configuration

Jettison of the Launch Escape System after a Successful Launch

Jettison of the Launch Escape System after a Successful Launch

Full-Scale Mockup of the Service Module with Panels Off

Full-Scale Mockup of the Service Module with Panels Off

The CM Probe Slips into the LM's Dish-shaped Drogue, and 12 latches on the Docking Ring Engage, to Lock the Spacecraft Together, Airtight

The CM Probe Slips into the LM’s Dish-shaped Drogue, and 12 latches on the Docking Ring Engage

The Cabin Section of the Command Module being Assembled at North American Aviation

The Cabin Section of the Command Module being Assembled at North American Aviation

Command Module Elbow & Shoulder Clearance Problem

Command Module Elbow & Shoulder Clearance Problem

May 14

Space Rocket History #113 – Apollo: Command Module Design and Development 1963-1964

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…From the information they gathered on the existing technical problems, Disher and Tischler concluded that prospects were only one in ten that Apollo would land on the moon before the end of the decade….

The "big dish" at Canberra Australia

The “big dish” at Canberra Australia

11/16/63 Blkhouse 37, NASA new Manned Space Flight chief George Mueller briefed. JFK there 6 days before his death

11/16/63 Blkhouse 37, NASA new Manned Space Flight chief George Mueller briefed. JFK there 6 days before his death

Removing LM from S=IVB stage

Removing LM from S=IVB stage

Mar 18

Space Rocket History #105 – Saturn’s First Flight – SA-1 – Part 2

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No previous maiden launch had gone flawlessly, and the Saturn C-1 was considerably more complicated than any rocket launched thus far. Launch Operations Directorate officials gave the rocket a 75% chance of getting off the ground, and a 30% chance of completing the eight-minute flight…

LC-34 Block House Control Room

LC-34 Block House Control Room

Abe Silverstein, Director of Space Flight

Abe Silverstein, Director of Space Flight

Liftoff or Saturn SA-1

All Eight Engines Firing and Liftoff of Saturn SA-1

Saturn SA-1 on Launch Pad 34

Saturn SA-1 on Launch Pad 34

Saturn SA-1 Leaving the Pad

Saturn SA-1 Leaving the Pad

Saturn SA-1 in Flight.

The First Saturn (SA-1) in Flight.

The Michoud Facility near New Orleans

The Michoud Facility near New Orleans

Ground Breaking at MSC

Ground Breaking at MSC