<--- Back to Details
First PageDocument Content
Single-stage-to-orbit / Space access / Spacecraft propulsion / Lifting bodies / Lockheed Martin / Lockheed Martin X-33 / Reusable launch system / Aerospike engine / Crew Return Vehicle / Aerospace engineering / Space technology / Spaceflight
Date: 2007-08-29 09:39:41
Single-stage-to-orbit
Space access
Spacecraft propulsion
Lifting bodies
Lockheed Martin
Lockheed Martin X-33
Reusable launch system
Aerospike engine
Crew Return Vehicle
Aerospace engineering
Space technology
Spaceflight

Add to Reading List

Source URL: www.gao.gov

Download Document from Source Website

File Size: 873,61 KB

Share Document on Facebook

Similar Documents

L2 Natural Environment Summary by Nancy J. Lindsey Lockheed Martin Technical Operations September 1998

DocID: 1vlSK - View Document

Case Study: Lockheed Martin Challenges Determine the structure of a complex legacy ADA program. Use Case Understandâ„¢ was used for the following applications:

DocID: 1vd3C - View Document

F-35 Lightning II Program Public Release – Pentagon and Lockheed Martin Deliver 300th F-35 Aircraft F-35 Joint Program Office/Lockheed Martin F-35 Enterprise Ramps Up Production and Reduces Costs

DocID: 1v8Ku - View Document

An ILS Inspired Approach and Departure System Utilizing Monocular Vision H. Claus Christmann Graduate Research Assistant Georgia Institute of Technology, Atlanta, GA, USA Eric N. Johnson Lockheed Martin Associate Profess

DocID: 1v0KB - View Document

Cyber Scientific Test Language Peter Haglich1, Robert Grimshaw2, Steven Wilder2, Marian Nodine3, and Bryan Lyles4 1 Lockheed Martin Advanced Technology Laboratories, Virginia Beach, VA

DocID: 1uUSO - View Document