Filling the launch gap
Abstract
Vehicles proposed to fill the gap in the U.S. space program's space transport needs for the next decade resulting from the January Challenger disaster, are discussed. Prior to the accident, the Air Force planned to purchase a Complementary Expendable Launch Vehicle system consisting of 10 single-use Titan-34D7 rockets. Another heavy lift booster now considered is the Phoenix H. Commercial launch vehicle systems projected to be available in the necessary time frame include the 215,000-pound thrust 4000-pound LEO payload capacity NASA Delta, the 11,300-pound LEO payload capacity Atlas Centaur the first ICBM, and the all-solid propellant expendable 2000-pound LEO payload Conestoga rocket. Also considered is the man-rated fully reusable Phoenix vertical take-off and vertical-landing launch vehicle.
- Publication:
-
Space World
- Pub Date:
- May 1986
- Bibcode:
- 1986SpWd....5...24H
- Keywords:
-
- Earth Orbital Environments;
- Launch Vehicles;
- Nasa Space Programs;
- Space Transportation System;
- Challenger (Orbiter);
- Expendable Stages (Spacecraft);
- Research And Development;
- Rocket Engines;
- Space Commercialization;
- Launch Vehicles and Space Vehicles