# Presentation: 830673

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**Notes:**
Name of Image: Saturn-Nova Comparison 
MIX #:9902050
NIX #:MSFC-01061 
Date of Image: 1962                                          
Category:Concepts 
Full Description: 
                                         In this artist's concept from 1962, a proposed Nova
                                         rocket, shown at right, is compared to a Saturn
                                         C-1, left, and a Saturn C-5, center. Marshall Space
                                         Flight Center directed studies of Nova
                                         configurations from 1960 to 1963 as a means of
                                         achieving a manned lunar landing with a direct
                                         flight to the moon. Various configurations of the
                                         vehicle were examined, the largest a five-stage
                                         vehicle using eight F-1 engines in the first stage.
                                         Although the program was effectively cancelled in
                                         1962 when NASA planners chose the lunar-orbital
                                         rendezvous mode, the proposed F-1 engine would
                                         eventually be used to propel the first stage of the
                                         Saturn V launch vehicle in the Apollo program. 

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**Notes:**
Name of Image:                                                  Modular Nova Concept 
MIX #:9902051
NIX #:MSFC-01062 
Date of Image:1960
Category:                                                  Concepts 
                            Full Description: 
                                         This artist's concept illustrates the Nova launch
                                         vehicle concept. By clustering the engines and
                                         stages of the Saturn C-3 (left), a Nova launch
                                         vehicle would be able to launch a 50-ton escape
                                         payload (center). Increases in payload capacity
                                         through an upper stage (right) could launch a
                                         70-ton escape payload, such as the lunar
                                         spacecraft shown on the far right. The Nova launch
                                         vehicle was considered by Marshall Space Flight
                                         Center from 1960 to 1963 as a means to achieve
                                         a manned lunar landing with a direct flight to the
                                         moon. 

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## Photo Number IV-130-H3

- Feature Name:   Clavius
- Feature Latitude:   58.8°S
- Feature Longitude:  14.1°W
- Size:   245 km
- Sun Angle:   81.3°
- Spacecraft Altitude:   3574.83 km
- Medium Photo Center Latitude:   65.02°S
- Medium Photo Center Longitude:  25.85°W

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## Apollo 16 Lunar Landing

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## Apollo 15 Imbrium Basin Impact Melt

**Apollo 15 Imbrium Basin Impact Melt**

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## Apollo 15 “Genesis Rock”

**Apollo 15 “Genesis Rock”**

## Apollo 15 Moon Rock Sampling

**Apollo 15 Moon Rock Sampling**

## Apollo 16 Anorthosite

**Apollo 16 Anorthosite**

## Apollo 17 Orange Glass in Soil

**Apollo 17 Orange Glass in Soil**

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