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NASA Armstrong Fact Sheet: Dryden's Contributions to Spaceflight
February 28, 2014
 

X-15 just after launchThe X-15 #2 (56-6671) launches away from the B-52 mothership with its rocket engine ignited. The Armstrong Flight Research Center in California's Mojave Desert is NASA's lead installation for atmospheric flight research. Armstrong performs research, development and verification of advanced aerospace technologies for production, prototype, or experimental vehicles.

NASA Armstrong has played a significant role in NASA's human space flight programs. Armstrong's major past contributions as the Dryden Flight Research Center and present contributions to America's access to space date from the late 1950s and continue today as NASA looks toward resuming human exploration of the moon and the solar system.

Research with the X-15 rocket plane in the 1960s contributed to space exploration in several areas, including:

  • Reaction control systems for attitude control and maneuvering outside the Earth's atmosphere.
  • Life support systems, such as practical full-pressure suits for pilot protection.
  • Inertial navigation systems for operation in low and high dynamic flight conditions.
  • Flight control mechanisms that could control a vehicle in high and low dynamic flight conditions as well as gravity-free environments.

Lunar Landing Research Vehicle (LLRV) in flightThe Lunar Landing Research Vehicle (LLRV) number 1 is shown in flight. The Lunar Landing Research Vehicle (LLRV) investigated vehicle control and landing capabilities in zero dynamic pressure and near weightlessness, analog fly-by-wire control, and trained astronauts to safely land an unconventional vehicle in those conditions.

The family of wingless lifting bodies flown in the late 1960s and early 1970s enabled us to investigate energy management techniques for atmospheric re-entry and controlled descent to a landing in a vehicle without wings or power.

The F-8 Digital Fly-By-Wire project demonstrated digital computer control of aircraft flight controls, which led to lighter weight, greater redundancy, and more precision. The project also flight-validated the computers used in the Shuttle's flight control system, and resolved pilot-induced oscillation tendencies in digital controls through the development of suppression filters.

Space Shuttle Endeavour and SCA 747 taking off from Dryden. The Space Shuttle Endeavour, mounted securely atop one of NASA's modified Boeing 747 Shuttle Carrier Aircraft, left NASA's Dryden Flight Research Center at Edwards, CA, at sunrise on Friday, June 28, 2002. NASA photo. Research with the triple-sonic YF-12 led to a central airborne performance analyzer that became the basis for vehicle health monitoring system used on the Space Shuttles.

The Space Shuttle Approach and Landing Tests validated both the ability of the modified Boeing 747 Shuttle Carrier Aircraft to carry the shuttle and the approach and precision landing of the unpowered Shuttle on the main and lakebed runways at Edwards Air Force Base.

Dryden flight-validated the Shuttle's solid rocket booster parachute recovery system in the 1980s, and the effectiveness of the Shuttle's drag parachute a decade later.

Dryden's Flight Loads Laboratory also validated the integrity of the Shuttle's structure under intense thermal conditions.

Dryden conducted flight tests of the Shuttle's Thermal Protection System, using F-104 and F-15 aircraft to test shuttle TPS tiles under various aerodynamic and atmospheric conditions.

Illustration of Crew Escape Vehicle Launch Abort Vehicle graphic. NASA Illustration Tests on a modified CV-990 led to improved Shuttle tires and brakes, higher crosswind landing limits, and resurfacing of the Kennedy runway for better tire wear.

Tests flown on Dryden's F-15B research testbed aircraft in 2005 investigated the trajectory of insulating foam that separates from the Shuttle's external tank on ascent.

Looking to the future, the same skills that have enabled NASA researchers and pilots to unlock aeronautical secrets for decades have been called upon to accelerate the development of NASA's exploration systems.

NASA Dryden led the integration and flight test operations of an advanced system that could safely abort a launch of the Orion Multi-Purpose Crew Vehicle if problems develop that are hazardous to the crew. The highly successful flight test occurred at the U.S. Army's White Sands Missile Range in New Mexico in May 2010.

In addition to the preliminary definition and planning for the Orion launch abort systems flight test, Dryden's responsibilities for the Orion vehicle included procurement of the abort test rocket booster; flight test article and abort test booster integration; flight test article design, assembly, integration, and testing; and independent analysis and oversight of prime contractors' flight test articles.

Dryden is expected to be involved in future landing and recovery tests, flight re-entry and landing profiles, and range safety requirements and integration for the Orion module.
 

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Page Last Updated: February 28th, 2014
Page Editor: Yvonne Gibbs