The nuclear electric propulsion (NEP) concept design developed in support of the Space Transfer Concepts and Analysis for Exploration Missions (STCAEM) study is presented. The evolution of the NEP concept is described along with the requirements, guidelines, and assumptions for the design. Operating modes and options are defined and a systems description of the vehicle is presented. Artificial gravity configuration options and space and ground support systems are discussed. Finally, an implementation plan is presented which addresses technology needs, schedules, facilities and costs
The tethered satellite system (TSS) was envisioned as a means of extending a satellite from its base...
A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no fligh...
This report analyzes and presents a preliminary design for an experimental hypersonic vehicle. This ...
This document presents the solar electric propulsion (SEP) concept design developed as part of the S...
The cryogenic/aerobrake (CAB) and the cryogenic all-propulsive (CAP) concept designs developed in su...
This document presents the nuclear thermal rocket (NTR) concept design developed in support of the S...
This document presents trade studies and reference concept designs accomplished during a study of Sp...
A long life, single stage, reverse Brayton cycle cryogenic cooler is being developed for application...
This paper presents a design of a military transport aircraft capable of carrying 800,000 lbs of pay...
The Shuttle Upgrade program is a continuing improvement process to enable the Space Shuttle to be an...
The spacecraft design project was part of AE-4871, Advanced Spacecraft Design. The project was inten...
The design, construction, and operation of a low-Earth orbit space station poses unique challenges f...
The Marshall Space Flight Center has a rich heritage of launch vehicles that have used aerodynamic s...
The Real-Time Failure Control (RTFC) program involves development of a failure detection algorithm, ...
Activities carried out during this reporting period are summarized. Much of the work undertaken invo...
The tethered satellite system (TSS) was envisioned as a means of extending a satellite from its base...
A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no fligh...
This report analyzes and presents a preliminary design for an experimental hypersonic vehicle. This ...
This document presents the solar electric propulsion (SEP) concept design developed as part of the S...
The cryogenic/aerobrake (CAB) and the cryogenic all-propulsive (CAP) concept designs developed in su...
This document presents the nuclear thermal rocket (NTR) concept design developed in support of the S...
This document presents trade studies and reference concept designs accomplished during a study of Sp...
A long life, single stage, reverse Brayton cycle cryogenic cooler is being developed for application...
This paper presents a design of a military transport aircraft capable of carrying 800,000 lbs of pay...
The Shuttle Upgrade program is a continuing improvement process to enable the Space Shuttle to be an...
The spacecraft design project was part of AE-4871, Advanced Spacecraft Design. The project was inten...
The design, construction, and operation of a low-Earth orbit space station poses unique challenges f...
The Marshall Space Flight Center has a rich heritage of launch vehicles that have used aerodynamic s...
The Real-Time Failure Control (RTFC) program involves development of a failure detection algorithm, ...
Activities carried out during this reporting period are summarized. Much of the work undertaken invo...
The tethered satellite system (TSS) was envisioned as a means of extending a satellite from its base...
A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no fligh...
This report analyzes and presents a preliminary design for an experimental hypersonic vehicle. This ...