Development of the Saturn Space Vehicle [PDF]
Space science - launch vehicle - saturn ...
Lange, O. H.
core +1 more source
The development of cryogenic storage systems for space flight [PDF]
Development of cryogenic storage systems for manned space ...
Allgeier, R. K., Jr. +3 more
core +1 more source
Saturn i launch vehicle sa-10 and launch complex 37b functional systems description. volume x- separation and flight termination systems functional description, index of finding numbers, and mechanical schematics [PDF]
Inflight stage separation and flight termination system for Saturn I /SA-10/ launch ...
core +1 more source
STS payload ground handling mechanism at John F. Kennedy Space Center [PDF]
, 1985 The payload ground handling mechanism (PGHM), which lifts payloads out of the payload canister that brings them to the launch pad, is described. The PGHM then loads the payloads into the orbiter through the open payload bay doors.
Cassisi, V., Tatem, B. C., Jr.
core +1 more source
Diffusion bonding of titanium to simulate S-1C fuel tankage components [PDF]
Developing fabrication methods for diffusion bonding of titanium alloys to meet SIC fuel tank design ...
Irvine, C. N.
core +1 more source
Orbital Maneuvering system design evolution [PDF]
, 1985 Preliminary design considerations and changes made in the baseline space shuttle orbital maneuvering system (OMS) to reduce cost and weight are detailed.
Gibson, C., Humphries, C.
core +1 more source
Space shuttle orbiter test flight series [PDF]
The proposed studies on the space shuttle orbiter test taxi runs and captive flight tests were set forth. The orbiter test flights, the approach and landing tests (ALT), and the ground vibration tests were cited.
Garrett, D., Gordon, R., Jackson, R. B.
core +1 more source
Variable gravity research facility [PDF]
Spin and despin requirements; sequence of activities required to assemble the Variable Gravity Research Facility (VGRF); power systems technology; life support; thermal control systems; emergencies; communication systems; space station applications ...
Allan, Sean +9 more
core +1 more source
Launch vehicle performance using metallized propellants [PDF]
Metallized propellant propulsion systems are considered as replacements for the solid rocket boosters and liquid sustainer stages on the current launch vehicles: both the Space Transportation System (STS) and the Titan 4.
Palaszewski, Bryan A., Powell, Richard
core +1 more source
Systems design analysis applied to launch vehicle configuration [PDF]
As emphasis shifts from optimum-performance aerospace systems to least lift-cycle costs, systems designs must seek, adapt, and innovate cost improvement techniques in design through operations.
Ryan, R., Verderaime, V.
core +1 more source