Caleb launch vehicle on loading trolley |
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| Function | Expendable launch system Sounding rocket Anti-satellite weapon |
|---|---|
| Manufacturer | US Navy |
| Country of origin | United States |
| Size | |
| Height | 4.9 metres (16 ft) |
| Diameter | 0.6 metres (2 ft 0 in) |
| Mass | 1,350 kilograms (3,000 lb) |
| Stages | One (test) Two (test) Four (unflown) |
| Capacity | |
| Payload to LEO |
7 kilograms (15 lb) |
| Launch history | |
| Status | Retired |
| Launch sites | Point Arguello San Nicolas |
| Total launches | 2 Caleb 2 SIP 3 Hi-Hoe |
| Successes | 1 Caleb (1 stage) 2 SIP 1 Hi-Hoe |
| Failures | 1 Caleb 2 Hi-Hoe |
| Maiden flight | Caleb: 1960-07-28 SIP: 1961-10-01 Hi-Hoe: 1961-10-05 |
| Last flight | Caleb: 1960-10-24 SIP: 1962-05-05 Hi-Hoe: 1962-07-25 |
The NOTS-EV-2 Caleb, also known as NOTS-500, Hi-Hoe and SIP was an expendable launch system, which was later used as a sounding rocket and prototype anti-satellite weapon. It was developed by the United States Navy Naval Ordinance Test Station (NOTS)[1] as a follow-up to the NOTS-EV-1 Pilot, which had been abandoned following ten consecutive launch failures.[2] Two were launched in July and October 1960, before the cancellation of the project.[1] Following cancellation, two leftover Calebs were used in the Satellite Interceptor Program, or SIP, whilst three more were used as sounding rocktets, under the designation Hi-Hoe.[1] These derivatives flew until July 1962, when the Hi-Hoe made its final flight.
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The Caleb was originally designed as a fast-response orbital launch system, to place small reconnaissance satellites, and other military payloads, into orbit at short notice.[3] The orbital configurations were four-stage vehicles, whilst test launches used one and two stage configurations. The project was cancelled due to pressure from the United States Air Force, who were responsible for all other orbital launches conducted by the US military, and no attempts to launch the vehicle into orbit were made.[1]
Caleb was an air-launched rocket, with its two launches being conducted from F4D Skyray #747, the same aircraft used in the Pilot trials.[4] Hi-Hoe was also air-launched, however it was released from an F4H Phantom II, which provided greater performance.[3] SIP launches were conducted from a ground launch pad on San Nicolas Island.[5] The aircraft used for the airborne launches took off from Point Arguello, which later became part of Vandenberg Air Force Base.[5]
The Caleb made its maiden flight, in a single-stage test configuration,[4] on 28 July 1960.[6] Its second flight was made on 24 October of the same year,[6] and used a two-stage configuration. It was unsuccessful, due to the second stage's failure to ignite.[4] Both test launches were suborbital.[7]
Both SIP launches used the two stage configuration. The first was conducted on 1 October 1961. It was successful and reached an apogee of 20 kilometres (12 mi). The second test, launched on 5 May 1962 was also successful, and reached the same apogee.[5] The three Hi-Hoe launches were conducted on 5 October 1961, and 26 March and 25 July 1962.[6] On the first two launches the second stage failed to ignite,[4] however the third was successful, and reached an apogee of 1,166 kilometres (725 mi).[5][6]
Despite the program's turn torwards success, the project was cancelled soon after the final Hi-Hoe test, the Department of Defense choosing to concentrate on the U.S. Air Force's Blue Scout sounding rocket program.[7]
| Date/Time (GMT) | Rocket | S/N | Outcome | Remarks[5] |
|---|---|---|---|---|
| 1960-07-28 | Caleb | TV-1 | Success | Single stage |
| 1960-10-24 | Caleb | TV-2 | Failure | Second stage failed to ignite |
| 1961-10-01 | SIP | SIP-1 | Success | Ground launch |
| 1961-10-05, 19:10 | Hi-Hoe | NC17.116 | Failure | Second stage failed to ignite |
| 1962-03-26, 19:03 | Hi-Hoe | NC17.121 | Failure | Second stage failed to ignite |
| 1962-05-05 | SIP | SIP-2 | Success | Ground launch |
| 1962-07-25, 15:41 | Hi-Hoe | NC17.117 | Success |
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