516
15 System Testing and Validation Technology of Lunar Lander
along with development of deep space exploration method, the requirements for test
methodology and test system are also more and more complicated and continuous
optimization in terms of accuracy, convenience and cost-effective of simulation is
also necessary.
References
1. Thomas CO, Donald EH (1967) Operational features of the Langley Lunar landing research
facility[R]. National Aeronautics and Space Administration, Washington DC
2. Donald RB, Gene JM (1965) Design and operational characteristics of a Lunar-landing research
vehicle[R]. National Aeronautics and Space Administration, Washington DC
3. Caluin RJ (1966) Operational experience with the electronic flight control systems of a Lunarlanding research vehicle[R]. National Aeronautics and Space Administration, Washington DC
4. Ulysse JB (1968) Evaluation of a full-scale Lunar-gravity simulator by comparison of landingimpact tests of a full-scale and a 1/6-scale Model[R]. National Aeronautics and Space
Administration, Washington DC
5. Ulysse JB (1965) Model investigation of technique for conducting full-scale landing-impact tests
at simulated lunar gravity[R]. National Aeronautics and Space Administration, Washington DC
6. William FR (1972) Apollo experience report Lunar module landing gear subsystem[R]. National
Aeronautics and Space Administration, Washington DC
7. Ulysse JB (1969) Full-scale Dynamic landing-impact investigation of a prototype Lunar module
landing gear [R]. National Aeronautics and Space Administration, Washington DC
8. Stanley PW (1973) Apollo experience report Lunar module structural subsystem [R]. National
Aeronautics and Space Administration, Washington DC
9. Thomas JT (1972) Apollo experience report thermal protection from engine-plume environments[R]. National Aeronautics and Space Administration, Washington DC
15 System Testing and Validation Technology of Lunar Lander
along with development of deep space exploration method, the requirements for test
methodology and test system are also more and more complicated and continuous
optimization in terms of accuracy, convenience and cost-effective of simulation is
also necessary.
References
1. Thomas CO, Donald EH (1967) Operational features of the Langley Lunar landing research
facility[R]. National Aeronautics and Space Administration, Washington DC
2. Donald RB, Gene JM (1965) Design and operational characteristics of a Lunar-landing research
vehicle[R]. National Aeronautics and Space Administration, Washington DC
3. Caluin RJ (1966) Operational experience with the electronic flight control systems of a Lunarlanding research vehicle[R]. National Aeronautics and Space Administration, Washington DC
4. Ulysse JB (1968) Evaluation of a full-scale Lunar-gravity simulator by comparison of landingimpact tests of a full-scale and a 1/6-scale Model[R]. National Aeronautics and Space
Administration, Washington DC
5. Ulysse JB (1965) Model investigation of technique for conducting full-scale landing-impact tests
at simulated lunar gravity[R]. National Aeronautics and Space Administration, Washington DC
6. William FR (1972) Apollo experience report Lunar module landing gear subsystem[R]. National
Aeronautics and Space Administration, Washington DC
7. Ulysse JB (1969) Full-scale Dynamic landing-impact investigation of a prototype Lunar module
landing gear [R]. National Aeronautics and Space Administration, Washington DC
8. Stanley PW (1973) Apollo experience report Lunar module structural subsystem [R]. National
Aeronautics and Space Administration, Washington DC
9. Thomas JT (1972) Apollo experience report thermal protection from engine-plume environments[R]. National Aeronautics and Space Administration, Washington DC