Mars Sample Recovery Helicopter: Rotorcraft to Retrieve the First Samples from the Martian Surface
PRACTICAL CONCEPTUAL DESIGN OF QUIETER URBAN VTOL AIRCRAFT
PRACTICAL CONCEPTUAL DESIGN OF QUIETER URBAN VTOL AIRCRAFT
Observations from Exploration of VTOL Urban Air Mobility Designs
Integrated Aeromechanics with Three-Dimensional Solid-Multibody Structures
Powerplant Design and Performance Analysis of a Manned All-Electric Helicopter
INVESTIGATION OF MAXIMUM BLADE LOADING CAPABILITY OF LIFT-OFFSET ROTORS
EXPLORATION OF CONFIGURATION OPTIONS FOR A LARGE CIVIL COMPOUND HELICOPTER
Application of Climate Impact Metrics to Civil Tiltrotor Design
UAS Integration into the NAS: An Examination of Baseline Compliance in the Current Airspace System
Wind Tunnel Measurements of Full-Scale UH-60A Rotor Tip Vortices
REQUIREMENTS FOR A HYDROGEN POWERED ALL-ELECTRIC MANNED HELICOPTER
Orion Capsule Handling Qualities for Atmospheric Entry
NDARC - NASA Design and Analysis of Rotorcraft: Theoretical Basis and Architecture
NDARC - NASA Design and Analysis of Rotorcraft: Validation and Demonstration
Design of a Slowed-Rotor Compound Helicopter for Future Joint Service Missions
A Densified Liquid Methane Delivery System for the Altair Ascent Stage
Subcooling for Long Duration In-Space Cryogenic Propellant Storage
Performance and Design Investigation of Heavy Lift Tilt-Rotor with Aerodynamic Interference Effects
Subcooling Cryogenic Propellants for Long Duration Space Exploration
An Assessment of the State-of-the-art in Multidisciplinary Aeromechanical Analyses
Requirements for Next Generation Comprehensive Analysis of Rotorcraft
Cryogenic Propellant Insulation System Design Tools for Mass Optimization of Space Vehicles
The Pfaff/Cauchy derivative identities and Hurwitz type extensions
Orion Entry, Descent and Landing Performance and Mission Design AIAA Paper