May 04

Space Rocket History #159 – Zond 6

Trouble began on the sixth day of the flight, November 17. The capsule developed an atmospheric  leak, the pressure first dropping from 760 to 380 mm of Mercury.  With the drop in cabin pressure all the animal test subjects died.  It would have killed any Cosmonaut not wearing a spacesuit.

Proton-K with 7K-L1

Proton-K with 7K-L1

Zone 6 mission profile

Zone 6 mission profile

Zond 6 Double-dip reentry

Zond 6 Double-dip reentry

Mar 16

Space Rocket History #153 – Zond 5 – Tortoises in Space & Nasa Stennis

The first attempt for a Zond 4 follow-up launched on April 22.  It failed when the Launch Escape System sent an erroneous abort command at T+260 seconds and shut down the Proton booster’s second stage. The escape rocket fired and pulled the descent module to safety.

Zond 5

Zond 5

Zond 5 Recovery

Zond 5 Recovery Indian Ocean

Scientist observing lunar Tortoises

Scientist observing lunar Tortoises

Feb 25

Space Rocket History #150 – Apollo 6: Pogo and the Tang Ceremony

The success of Apollo 4 gave good reason to believe that the Saturn V could be trusted to propel men into space. But NASA pushed on with its plans for a second unmanned booster flight, primarily to give the Pad 39 launch team another rehearsal before sending men into deep space on the Saturn V.  The mission was called Apollo 6…

Apollo 6 patch

Apollo 6 patch

Lunar Test Article

Lunar Test Article

Apollo 6 launch

Apollo 6 launch

Exhaust plume of Apollo 6

Exhaust plume of Apollo 6

Interstage falling away

Interstage falling away

Apollo 6 splashdown and recovery

Apollo 6 splashdown and recovery

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

May 21

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

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

…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

May 07

Space Rocket History #112 – Apollo: Headquarters

“The contractor role in Houston was not very firm. Frankly, they didn’t want us. There were two things against us down there. Number one, it was a Headquarters contract, and it was decreed that the Space Centers shall use GE for certain things; and number two they considered us (meaning GE) to be  Headquarters spies.”  Edward S. Miller of General Electric.

GE Employees Monitor Activities of a Spacecraft Test

GE Employees Monitor Activities of a Spacecraft Test

Comparison of Spacecraft and Launch Vehicles Configurations

Comparison of Spacecraft and Launch Vehicles Configurations

Apollo Tracking Network

Apollo Tracking Network

Apr 23

Space Rocket History #110 – Early Apollo Command Module Design

The Apollo contract specified a shirt-sleeve environment. For this reason, North American was told not to include in its design a hatch that opened by explosives, like Mercury’s. An accidentally blown hatch in space would cause an instant vacuum and certain death for an astronaunt not wearing his pressure suit.

Major parts of the CM Structure

Major parts of the CM Structure

NAA Apollo Team Storms, Paup, and Feltz

NAA Apollo Team Storms, Paup, and Feltz

Carpenter, Glenn, & Schirra in a full-scale mock up of the CM

Carpenter, Glenn, & Schirra in a full-scale mock up of the CM

The Impact Facility at NAA

The Impact Facility at NAA

Interior of a partial full-scale mockup of CM

Interior of a partial full-scale mockup of CM

Complete Apollo Family

Complete Apollo Family