North American F-100-F airplane, equipped with thrust reversers, full scale wind tunnel test. 3/4 front view of F-100-F airplane with North American Aviation thrust reverser. On standard 40x80 struts landing gear down. Mark Kelly, branch chief in photo.

This is a photograph of Dr. von Braun, taken in 1961, visiting North American Aviation's Space and Information Systems Division in Downey, California.

Dr. Wernher von Braun, Director of the Marshall Space Flight Center (MSFC), during his tour of the Space information Division of North American Aviation (NAA) in Downey, California, where the Saturn SII stage was developed.

A North American Aviation A-5A Vigilante (Navy serial number 147858/NASA tail number 858) arrived from the Naval Air Test Center, Patuxent River, MD, on December 19, 1962, at the NASA Flight Research Center (now, Dryden Flight Research Center, Edwards, CA). The Center flew the A-5A in a year-long series of flights in support of the U.S. supersonic transport program. The Center flew the aircraft to determine the let-down and approach conditions of a supersonic transport flying into a dense air traffic network. With the completion of the research flights, the Center sent the A-5A back to the Navy on December 20, 1963.

A North American Aviation A-5A Vigilante (Navy serial number 147858/NASA tail number 858) arrived from the Naval Air Test Center, Patuxent River, MD, on December 19, 1962, at the NASA Flight Research Center (now, Dryden Flight Research Center, Edwards, CA). The Center flew the A-5A in a year-long series of flights in support of the U.S. supersonic transport program. The Center flew the aircraft to determine the let-down and approach conditions of a supersonic transport flying into a dense air traffic network. With the completion of the research flights, the Center sent the A-5A back to the Navy on December 20, 1963.

The members of the prime crew of the first manned Apollo space flight Apollo/Saturn 204 (AS-204) inspect spacecraft equipment during a tour of North American Aviation's (NAA) Downey facility. In the foreground, left to right, are astronauts Roger B. Chaffee, Virgil I. Grissom, and Edward H. White, II. NAA engineers and technicians are in the background. NORTH AMERICAN AVIATION, INC., DOWNEY, CA B&W

The North American Aviation XB-70 triple-sonic bomber prototype aircraft No. 1. NASA used the pre-production bomber for high-speed research in the mid-1960s.

S66-53655 (1966) --- High angle view of Apollo Spacecraft 012 Command Module looking toward +Z axis during pre-shipping operations in south air lock of Systems Integration and Checkout Facility.

S68-46591 (1968) --- Artist's concept of the Apollo Command and Service Modules with call-outs. Photo credit: NASA

NASA research pilot Jack McKay was injured in a crash landing of the X-15 #2 on November 9, 1962. Following the launch from the B-52 to begin flight 2-31-52, he started the X-15's rocket engine, only to discover that it produced just 30 percent of its maximum thrust. He had to make a high-speed emergency landing on Mud Lake, NV, without flaps but with a significant amount of fuel still in the aircraft. As the X-15 slid across the lakebed, the left skid collapsed; the aircraft turned sideways and flipped onto its back. McKay suffered back injuries but was eventually able to resume X-15 pilot duties, making 22 more flights. The X-15 was sent back to North American Aviation and rebuilt into the X-15A-2.

This illustration, with callouts, is of the Saturn V SII (2nd Stage) developed by the Space Division of North American Aviation under the direction of the Marshall Space Flight Center. The 82-foot-long and 33-foot-diameter S-II stage utilized five J-2 engines, each with a 200,000-pound thrust capability. The engine used liquid oxygen and liquid hydrogen as its propellants.

Navaho in flight, 1957. Navaho is a surface-to-surface missile developed by North American Aviation under the U.S. Air Force Navaho Program. The Navaho engine was an improvement of the V-2 engine. Though program began in March 1946 and was cancelled in July 1957, the research to develop the Navaho engine contributed to the development of the Redstone, Jupiter, Thor, and ATLAS engines.

This photograph shows a test firing of the the Saturn V S-II (second) stage at the Mississippi Test Facility's (MTF) S-II test stand. When the Saturn V booster stage (S-IC) burns out and drops away, power for the Saturn will be provided by the 82-foot-long and 33-foot-diameter S-II stage. Developed by the Space Division of North American Aviation under the direction of the Marshall Space Flight Center, the stage utilized five J-2 engines, each producing 200,000 pounds of thrust. The engines used liquid oxygen and liquid hydrogen as propellants. Static test of ground test versions of the S-II stage were conducted at North American Aviation's Santa Susana, California test site. All flight stages were tested at the Mississippi Test Facility, Bay St. Louis, Mississippi. MTF was renamed to the National Space Technology Laboratory (NSTL) in 1974 and later to the Sternis Space Center in May 1988.

This photograph shows the Saturn V S-II (second) stage being hoisted at the S-II-A2 test stand at the Mississippi Test Facility (MTF). When the Saturn V booster stage (S-IC) burns out and drops away, power for the Saturn will be provided by the 82-foot-long and 33-foot-diameter S-II stage. Developed by the Space Division of North American Aviation under the direction of the Marshall Space Flight Center, the stage utilized five J-2 engines, each producing 200,000 pounds of thrust. The engines used liquid oxygen and liquid hydrogen as propellants. Static test of ground test versions of the S-II stage were conducted at North American Aviation's Santa Susana, California test site. All flight stages were tested at the Mississippi Test Facility, Bay St. Louis, Mississippi. MTF was renamed to the National Space Technology Laboratory (NSTL) in 1974 and later to the Sternis Space Center in May 1988.

This photograph shows a test firing of the the Saturn V S-II (second) stage at the Mississippi Test Facility's (MTF) S-II test stand. When the Saturn V booster stage (S-IC) burns out and drops away, power for the Saturn will be provided by the 82-foot-long and 33-foot-diameter S-II stage. Developed by the Space Division of North American Aviation under the direction of the Marshall Space Flight Center, the stage utilized five J-2 engines, each producing 200,000 pounds of thrust. The engine used liquid oxygen and liquid hydrogen as its propellants. Static test of ground test versions of the S-II stage were conducted at North American Aviation's Santa Susana, California test site. All flight stages were tested at the Mississippi Test Facility, Bay St. Louis, Mississippi. The MTF was renamed to the National Space Technology Laboratory (NSTL) in 1974 and later to the Sternis Space Center (SSC) in May 1988.

S67-23078 (27 Jan. 1967) --- Three astronauts (later to be named the Apollo 9 prime crew) in Apollo spacecraft 101 Command module during Apollo crew compartment fit and function test. Left to right are astronauts James A. McDivitt, David R. Scott, and Russell L. Schweickart.

S66-49181 (August 1966) --- The three crew members for the Apollo-Saturn 204 (AS-204) mission check out the couch installation on the Apollo Command Module (CM) at North American's Downey facility. Left to right in their pressurized space suits are astronauts Virgil I. Grissom, Roger B. Chaffee and Edward H. White II. Editor's Note: The three astronauts died in a fire on the launch pad, Jan. 27, 1967.

This Saturn V S-II (second) stage is being lifted into position for a test at the Vehicle Assembly Building at the Kennedy Space Center. When the Saturn V booster stage (S-IC) burned out and dropped away, power for the Saturn was provided by the 82-foot-long and 33-foot-diameter S-II stage. Developed by the Space Division of North American Aviation under the direction of the Marshall Space Flight Center, the stage utilized five J-2 engines, each producing 200,000 pounds of thrust. The engines used liquid oxygen and liquid hydrogen as propellants. The towering 363-foot Saturn V was a multi-stage, multi-engine launch vehicle standing taller than the Statue of Liberty. Altogether, the Saturn V engines produced as much power as 85 Hoover Dams.

Astronaut Virgil I. Grissom and other members of the first Apollo Crew inspect spacecraft equipment during a visit to NAA. NAA, INC., DOWNEY, CA B&W

S66-41852 (1966) --- Spacecraft 012 looking toward -Y axis during installation of heat shield. Note uprighting system compressor in aft bay, at right, and Reaction Control System (RCS) valve module panel, center of photo.

A Wright Aeronautical XRJ47-W-5 ramjet installed in a test chamber of the National Advisory Committee for Aeronautics’ (NACA) new Propulsion Systems Laboratory at the Lewis Flight Propulsion Laboratory. Construction of the facility had only recently been completed, and NACA engineers were still testing the various operating systems. The Propulsion Systems Laboratory was the NACA’s most powerful facility for testing full-scale engines in simulated flight altitudes. It contained two 14-foot diameter and 100-foot-long altitude chambers that ran parallel to one another with a control room in between. The engine being tested was installed inside the test section of one of the chambers, seen in this photograph. Extensive instrumentation was fitted onto the engine prior to the test. Once the chamber was sealed, the altitude conditions were introduced, and the engine was ignited. Operators in the control room could run the engine at the various speeds and adjust the altitude conditions to the desired levels. The engine’s exhaust was ejected into the cooling equipment. Two 48-inch diameter XRJ47-W-5 ramjets were used to power the North American Aviation Navaho Missile. The Navaho was a winged missile that was intended to travel up to 3000 miles carrying a nuclear warhead. It was launched using rocket booster engines that were ejected after the missile’s ramjet engines were ignited.

Astronauts McDivitt, Chaffee, White are shown in Spacecraft. NAA, INC., DOWNEY, CA B&W

Southwestern US, with Las Vegas, NV in foreground, taken by X-15 Hycon HR-236 Camera during flt. 2-39-70 on June 27, 1965.

Cutaway drawing of the North American X-15.

X-15A-2 with full scale ablative and external tanks installed parked in front of hangar. In June 1967, the X-15A-2 rocket-powered research aircraft received a full-scale ablative coating to protect the craft from the high temperatures associated with hypersonic flight (above Mach 5). This pink eraser-like substance, applied to the X-15A-2 aircraft (56-6671), was then covered with a white sealant coat before flight. This coating would help the #2 aircraft reach the record speed of 4,520 mph (Mach 6.7).

Cracked canopy glass on right side of X-15 #2 after flt. 2-21-37 on Nov. 9 1961. Robert White-pilot. First flight to mach 6.

Cutaway drawing of the North American X-15.

Three view art of the North American X-15.

X-15A-2 is rolled out of the paint shop after having the full scale ablative applied. In June 1967, the X-15A-2 rocket-powered research aircraft received a full-scale ablative coating to protect the craft from the high temperatures associated with hypersonic flight (above Mach 5). This pink eraser-like substance, applied to the X-15A-2 aircraft (56-6671), was then covered with a white sealant coat before flight. This coating would help the #2 aircraft reach the record speed of 4,520 mph (Mach 6.7).

X-15A-2 post flight photo showing heat damage from Mach 6.7 flight on 3 Oct 67. Flt. 2-53-97; pilot-Pete Knight.

In this photo of the M2-F1 lifting body and the Paresev 1B on the ramp, the viewer sees two vehicles representing different approaches to building a research craft to simulate a spacecraft able to land on the ground instead of splashing down in the ocean as the Mercury capsules did. The M2-F1 was a lifting body, a shape able to re-enter from orbit and land. The Paresev (Paraglider Research Vehicle) used a Rogallo wing that could be (but never was) used to replace a conventional parachute for landing a capsule-type spacecraft, allowing it to make a controlled landing on the ground.