Synonyms were used for:
launch vehicle
•
vehicle
Search without synonyms:
keywords:(launch vehicle)
50 Years of Mirror Technology Investment at NASA: From Hubble to JWST and Beyond
19304A MLRS, Missile Number 1135, Round Number V-103, 15 January 1980
19304B MLRS, Missile Number 1134, Round Number V-100, 8 January 1980
19304D MLRS, Missile Number 1130, Round Number V-99, 18 December 79
19304 MLRS Missile Numbers 1085, 1087, 1088, 1089, 1090, 1092, Round Numbers V-83 thru V-88
19306B MLRS, Missile Numbers 1058-1099, Round Numbers V-101 - V-102, 14 January 80
19308B MLRS, Missile Number 1125, Round Number V-98, 11 December 1979
19701A MLRS, Missile Numbers 068, 024, Round Numbers B-68, B-69, 5 January 1980
19701B MLRS, Missile Number 066, Round Number B-59
19701B MLSR, Missile Number 214, Round Number B-74, 18 January 1980
19704A MLRS, Missile Number 067, Round Number B-71, 7 January 80
19705B MLRS, Missile Numbers 331, 196, Round Numbers B-72, B-73, 11 January 1980
Abschlussbericht DIAMANT - Diaphragm Modelle, Analysen und Tests
Abschlussbericht DIAMANT - Diaphragm Modelle, Analysen und Tests
A comparison of iterative explicit guidance algorithms for space launch vehicles
A comparison of the vibration environment measured on the saturn flights with predicted values
Acoustics Research of Propulsion Systems
Advanced control systems for the Saturn V launch vehicle.
Advanced Planetary Probe Study Mid-term technical progress report
Advanced Systems Checkout Design Fourth Quarterly Progress Report, Mar. 30 - Jun. 29, 1966
Advanced systems checkout design Fourth quarterly progress report, Mar. 30 - Jun. 29, 1966
Aerodynamic Data for Calculation of Eldo-a Stationary in-Flight Loads and Loading Distribution
Aerodynamic heating tests of several variations of insulation system
Aeroelastic load growth effects on Saturn configurations
Aeroelastic Load Growth Effects on Saturn Configurations
A fault-tolerant architecture for launch vehicle guidance and control. II. Implementation
A fault-tolerant architecture for launch vehicle guidance and control. I. Requirement/architecture
Alignment of Sensors and Nutation Damper in the Eldo/Pas Satellite
A matrix-holzer analysis for bending vibrations of clustered launch vehicles.
An Airborne Pulse Counter and Serial Encoder
Analysis and Design of Space Vehicle Flight Control Systems. Volume I - Short Period Dynamics